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F., J13-180 Zhang, Z., J13-188 Sankar, L., J13-087 Sun, D., J13-155 Wang, H., J13-016 Zhangchun, T., J13-215 Sankararaman, S., J13-053 Sun, H., J13-059 Wang, J., J13-001 Zhao, L., J13-270 Sawant, S., J13-211 Sun, X., J13-155 Wang, L., J13-131 Zhenzhou, L., J13-215 Schatzman, D., J13-223 Sundararajan, T., J13-040 Wang, M., J13-163 Zhong, S., J13-036 Schmidt, S., J13-238 Sung, H.G., J13-146 Wang, P., J13-215 Zhong, X., J13-023 Schotté, J.S., J13-207 Sunny, M., J13-234 Wang, Q., J13-160 Zhou, L., J13-255 Schréder, W., J13-144 Suzuki, K., J13-196 Wang, X., J13-023 Zhu, M., J13-269 Schroter, D., J13-091 Swindeman, M., J13-089 Wang, X., J13-070 Zhu, W.J., J13-002 Schulz, V., J13-238 Syal, M., J13-083 Wang, Y., J13-024 Zingg, D., J13-126, J13-181, Seele, R., J13-136 Tafti, D., J13-011 Wang, Z., 513-092, J13-265 J13-257 Segal, C., J13-184 Takagi, T., J13-165 Wang, Z. J., J13-190 Segawa, T., J13-042 Tang, D., J13-031, J13-120, J13-258 Watkins, S., J13-137 AIAA JOURNAL Vol. 51, No. 12, December 2013 2013 Chronological Index DOI: 10.2514/1.J053095 J13-001 Transient Loads Control of a Variable Speed Rotor During J13-014 Validation of an Improved Experimental Method for Use in Lagwise Resonance Crossing. Dong Han, Joseph Wang, Edward C. Smith, Impedance Eduction. M. G. Jones and W. R. Watson, NASA Langley and George A. Lesieutre, Pennsylvania State University (51, 1, p. 20) Full Research Center (51, 1, p. 186) Full Paper based on AIAA Paper Paper J13-015 Development of a Particle—Particle Hybrid Scheme to J13-002 Hybrid Immersed Boundary Method for Airfoils with a Simulate Multiscale Transitional Flows. Rakesh Kumar, E. V. Titov, and Trailing-Edge Flap. Wei Jun Zhu, Tim Behrens, Wen Zhong Shen, and Jens D. A. Levin, Pennsylvania State University (51, |, p. 200) Full Paper based on Norkzr Sorensen, Technical University of Denmark, Denmark (51, 1, p. 30) AIAA Paper 2011-0625 Full Paper J13-016 Lower-Bound Analysis of Fiber-Reinforced Polymeric Laminated Cylindrical Shells. Hongtao Wang and James G. A. Croll, J13-003 Analytical and Numerical Study of Combustion Noise University College London, United Kingdom (51, 1, p. 218) Full Paper Through a Subsonic Nozzle. Ignacio Duran, Snecma, France; Stéphane Moreau, Université de Sherbrooke, Canada; and Thierry Poinsot, Institut de J13-017 Effects of Oxygen Enrichment on Scramjet Performance. Méchanique des Fluides de Toulouse, France (51, |, p. 42) Full Paper based on David J. Petty, Vincent Wheatley, Michael K. Smart, and Sarah A. Razzagqi, AIAA Paper University of Queensland, Australia (51, 1, p. 226) Full Paper J13-004 Adaptive Cartesian Immersed Boundary Method for J13-018 Simultaneous Iterative Method for Eigenpair Derivatives of Simulation of Flow over Flexible Geometries. Robert E. Harris, CFD Damped Systems. Huiging Xie, East China University of Science and Research Corporation (51, 1, p. 53) Full Paper based on AIAA Paper 2011- Technology, People’s Republic of China (51, 1, p. 236) Full Paper 3384 J13-019 Vortical Interactions Behind Deployable Vortex Generator J13-005 Mean Streamwise Centerline Velocity Decay and Entrain- for Airfoil Static Stall Control. G. Joubert and A. Le Pape, CNERA—The ment in Triangulaarnd Circular Jets. W. R. Quinn and M. Azad, St. Francis French Aerospace Lab, France; B. Heine, German Aerospace Center (DLR), Xavier University, Canada; and D. Groulx, Dalhousie University, Canada Germany; and S. Huberson, CNRS—Université de Poitiers-ENSMA, France (51, 1, p. 70) Full Paper based on AIAA Paper 2011-3087 (51, 1, p. 240) Full Paper based on AIAA Paper J13-020 Feedback Mechanism in Supersonic Laminar Cavity Flows. J13-006 Two-Dimensional Shovk-Wave/Boundary-Layer Interac- Weipeng Li, University of Tokyo, Japan; and Taku Nonomura, Akira Oyama, tion in the Presence of Entropy Layer. Volf Y. Borovoy, Ivan V. Egorov, and Kozo Fujii, Japan Aerospace Exploration Agency, Japan (51, 1, p. 253) Arkady S. Skuratov, and Irina V. Struminskaya, TsAG/. Russia (51, 1, p. 80) Full Paper based on AIAA Paper 2011-731 Note based on AIAA Paper J13-021 Master Formula for Geometrically Nonlinear Dynamic J13-007 Surrogate-Based Aerodynamic Shape Optimization by Instability of Shear Flexible Beams. B. Subba Ratnam and G. Venkateswara Variable-Resolution Models. Slawomir Koziel and Leifur Leifsson, Rao, Vardhaman College of Engineering, India; and G. Ranga Janardhana, Reykjavik University, Iceland (51, 1, p. 94) Full Paper based on AIAA Paper JNTU College of Engineering, India (51, 1, p. 257) Note J13-008 Investigation of Flows Around a Rudimentary Landing J13-022 Forced Vibration of Turbine Cascade Predicted by Gear with Advanced Detached-Eddy-Simulation Approaches. Zhixiang Transformation Techniques Considering Flow Compressibility. I! Lee, Xiao, Jian Liu, Kunyu Luo, Jingbo Huang, and Song Fu, Tsinghua University, SangJoon Shin, and Taehyoun Kim, Seoul National University, Republic of People’s Republic of China (51, 1, p. 107) Full Paper based on AIAA Paper Korea (51, 1, p. 262) Note 2012-2282 J13-023 Stabilization of a Mach 5.92 Boundary Layer by Two- J13-009 Derivative-Enhanced Variable Fidelity Surrogate Modeling Dimensional Finite-Height Roughness. Le Duan, Xiaowen Wang, and for Aerodynamic Functions. Wataru Yamazaki, Nagaoka University of Xiaolin Zhong, University of California, Los Angeles (51, |, p. 266) Note Technology, Japan; and Dimitri J. Mavriplis, University of Wyoming (51, 1, based on AIAA Paper p. 126) Full Paper based on AIAA Paper J13-024 Abort Separation of Launch Escape System Using J13-010 Hybrid Dimension-Reduction Method for Robust Design Aerodynamic Interference. Yunpeng Wang, /nstitute of Mechanics, China; Optimization. Hong-Shuang Li, Nanjing University of Aeronautics and and Hiroshi Ozawa, Hiroto Koyama, and Yoshiaki Nakamura, Nagoya Astronautics, People’s Republic of China; and Chao Ma, Shanghai Academy University, Japan (51, 1, p. 270) Note based on AIAA Paper of Spaceflight Technology, People’s Republic of China (51, 1, p. 138) Full J13-025 Comparison of Node-Centered and Cell-Centered Unstruc- Paper tured Finite-Volume Discretizations: Inviscid Fluxes. Boris Diskin, National Institute of Aerospace; and James L. Thomas, NASA Langley J13-011 Effect of Stroke Deviation on Forward Flapping Flight. Research Center (51, 1, p. 277) Erratum Kamal Viswanath and Danesh K. Tafti, Virginia Polytechnic Institute and State University (51, 1, p. 145) Full Paper J13-026 Probabilistic Analysis with Sparse Data. Mark McDonald, Lipscomb University, Kais Zaman, Bangladesh University of Engineering & J13-012 Postcritical Analysis of PrandtlPlane Joined-Wing Confi- Technology, Bangladesh; and Sankaran Mahadevan, Vanderbilt University gurations. Luciano Demasi, Rauno Cavallaro, and Alan Marquez Razon, San (51, 2, p. 281) Full Paper based on AIAA Paper 2009-2250 Diego State University (51, 1, p. 161) Full Paper J13-027 Aeolian Tones Generated by a Square Cylinder with a J13-013 Real-Time Estimation of Time-Varying Bending Modes Detached Flat Plate. Mohamed Sukri Mat Ali, Universiti Teknologi Using Fiber Bragg Grating Sensor Arrays. Hao Jiang, Bartel van der Veek, Malaysia, Malaysia; Con J. Doolan, University of Adelaide, Australia; and Daniel Kirk, and Hector Gutierrez, Florida Institute of Technology (51, 1, Vincent Wheatley, University of Queensland, Australia (51, 2, p. 291) Full p. 178) Full Paper Paper based on AIAA Paper 2011-2779 AIAA JOURNAL, VOL. 51, NO. 12: 2013 INDEX 3005 J13-028 Heated Helium to Simulate Surface Pressure Fluctuations J13-044 Hot-Wall Reentry Testing in Hypersonic Impulse Facilities. Created by Rocket Motor Plumes. J. Panda, N. J. Burnside, R. K. Fong, and F. Zander, R. G. Morgan, and U. Sheikh, University of Queensland, Australia; J. C. Ross, NASA Ames Research Center, and G. H. James and V. A. Fogt, D. R. Buttsworth, University of Southern Queensland, Australia; and P. R. NASA Johnson Space Center (51, 2, p. 302) Full Paper based on AIAA Paper Teakle, Teakle Composites, Australia (51, 2, p. 476) Full Paper 2011-2901 J13-045 Dynamic Elasticity Solution for the Transient Blast J13-029 Fluid Dynamics of Pitching and Plunging Flat Plate at Response of Sandwich Beams/Wide Plates. G. A. Kardomateas, Y. Frostig, Intermediate Reynolds Numbers. Chang-kwon Kang, Hikaru Aono, Yeon and C. N. Phan, Georgia Institute of Technology (51, 2, p. 485) Full Paper Sik Baik, Luis P. Bernal, and Wei Shyy, University of Michigan (51, 2, p. 315) Full Paper based on AIAA Paper 2009-4100 J13-046 Anisotropic hp-Adaptation Framework for Functional J13-030 Robust Gust Alleviation and Stabilization of Very Flexible Prediction. Marco Ceze and Krzysztof J. Fidkowski, University of Michigan Aircraft. Robert G. Cook and Rafael Palacios, /mperiail College, United (51, 2, p. 492) Full Paper Kingdom; and Paul Goulart, ETH Zurich (51, 2, p. 330) Full Paper J13-047 Synthetic Jets as a Boundery Vorticity Flux Control Tool. J13-031 Computational/Experimental Aeroelastic Study for a Joshua Yen and Noor A. Ahmed, University of New South Wales, Australia Horizontal-Tail Model with Free Play. Deman Tang and Earl H. Dowell, (51, 2, p. 510) Note Duke University (51, 2, p. 341) Full Paper J13-048 Development of an Alternative Delayed Detached-Eddy J13-032 Propagation of Uncertainty in Substructured Spacecraft Simulation Formulation Based on Elliptic Relaxation. Neil Ashton, Using Frequency Response. Daniel C. Kammer and Dimitri Krattiger, Alistair Revell, Robert Prosser, and Juan Uribe, University of Manchester, University of Wisconsin (51, 2, p. 353) Full Paper United Kingdom (51, 2, p. 513) Note J13-033 Atmospheric Plasma Thruster: Theory and Concept. A. Greig, C. H. Birzer, and M. Arjomandi, University of Adelaide, Australia (51, J13-049 High-Order Interface for Aeroacoustic Computation Using 2, p. 362) Full Paper Overset Grid. X. X. Chen and X. Zhang, University of Southampton, United Kingdom (51, 2, p. 519) Note J13-034 Large-Eddy Simutation of Heat Transfer Around a Square Cylinder Using Unstructured Grids. M. Boileau, F. Duchaine, and J.-C. J13-050 Optical Turbulence Model Sensitized to the Microscale Jouhaud, Centre Européen de Recherche et de Formation Avancée en Calcul Reynolds Number. Ji Ryong Cho, /nje University, Republic of Korea; Hyun Scientifique, France; and Y. Sommerer, Airbus Industries, 31060 Toulouse Tae Kim and Soo Sang Lee, Doosan DST, Republic of Korea; and Byung Seo Cedex 09, France (51, 2, p. 372) Full Paper Park and Eung Cheol Kang, Agency for Defense Development, Republic of Korea (51, 2, p. 523) Note J13-035 Design and Characterization of High-Bandwidth, Reso- nance Enhanced Pulsed Microactuators: A Parametric Study. John T. J13-051 Vortex Generator Flow Model Based on Self-Similarity. Solomon, Chase Foster, and Farrukh S. Alvi, Florida A&M University and Clara Marika Velte, Technical University ofD enmark, Denmark (51, 2, p. 526) Florida State University (51, 2, p. 386) Full Paper Note J13-036 New Fluidic-Oscillator Concept for Flow-Separation Control. V. Tesaf, Academy of Sciences of the Czech Republic, Czech J13-052 Aerodynamic Estimation of Annular Wings Based on Republic; and S. Zhong and F. Rasheed, University of Manchester, United Leading-Edge Suction Analogy. Adnan Maqsood, National University of Kingdom (51, 2, p. 397) Full Paper Sciences and Technology, Pakistan; and Tiauw Hiong Go, Nanyang Technological University, Republic of Singapore (51, 2, p. 529) Note J13-037 External Mean Flow Effects on Noise Radiation from Orthogonally Rib-Stiffened Aeroelastic Plates. F. X. Xin and T. J. Lu, Xi’an J13-053 Test Resource Allocation in Hierarchical Systems Using Jiaotong University, People’s Republic of China (51, 2, p. 406) Full Paper Bayesian Networks. Shankar Sankararaman, Kyle McLemore, and Sankaran Mahadevan, Vanderbilt University; and Samuel Case Bradford and Lee D. J13-038 Experimental Investigation of Base-Drag Reduction via Peterson, Jet Propulsion Laboratory, California Institute of Technology (51, Boundary-Layer Modification. Vibhav Durgesh and Jonathan W. Naughton, 3, p. 537) Full Paper University of Wyoming; and Stephen A. Whitmore, Utah State University (51, 2, p. 416) Full Paper based on AIAA Paper 2006-3186 J13-054 Aircraft Vortices in Stably Stratified and Weakly Turbulent Atmospheres: Simulation and Modeling. I. De Visscher, L. Bricteux, and G. J13-039 New Approach to Bounding Effective Properties of Random Winckelmans, Université catholique de Louvain, Belgium (51, 3, p. 551) Full Heterogeneous Materials. Zheng Ye and Wenbin Yu, Utah State University Paper (51, 2, p. 426) Full Paper based on AIAA Paper 2011-2160 J13-040 Simulations of High Altitude Tests for Large Area Ratio J13-055 Approximate Aeroelastic Modeling of Flapping Wings in Rocket Motors. R. Manikanda Kumaran and T. Sundararajan, /ndian Institute Hover. Abhijit Gogulapati, Peretz P. Friedmann, Eugene Kheng, and Wei of Technology, India; and D. Raja Manohar, Indian Space Research Shyy, University of Michigan (51, 3, p. 567) Full Paper Organization, India (51, 2, p. 433) Full Paper J13-056 Concept of Non-Ablative Thermal Protection System for J13-041 Optimizations Under Uncertainty Using Gradients, Hypersonic Vehicles. Yunfeng Liu and Zonglin Jiang, Chinese Academy of Hessians, and Surrogate Models. Markus P. Rumpfkeil, University of Sciences, People’s Republic of China (51, 3, p. 584) Full Paper based on AIAA Dayton (51, 2, p. 444) Full Paper based on AIAA Paper Paper J13-042 Flow Control on a NACA 4418 Using Dielectric-Barrier- J13-057 Transverse Waves in Simulated Liquid Rocket Engines. Discharge Vortex Generators. Timothy N. Jukes, Takehiko Segawa, and Charles T. Haddad and Joseph Majdalani, University of Tennessee Space Hirohide Furutani, National Institute of Advanced Industrial Science and Institute (51, 3, p. 591) Full Paper based on AIAA Paper 2011-6029 Technology, Japan (51, 2, p. 452) Full Paper based on AIAA Paper 2012-1139 J13-043 Predictions of Sound from Rough Wall Boundary Layers. J13-058 Method for Optimally Controlling Unsteady Shock W. Nathan Alexander and William J. Devenport, Virginia Polytechnic Institute Strength in One Dimension. Nathan D. Moshman, Garth V. Hobson, and and State University; and Stewart A. L. Glegg, Florida Atlantic University (51, Sivaguru S. Sritharan, Naval Postgraduate School (51, 3, p. 606) Full Paper 2, p. 465) Full Paper based on AIAA Paper 2011-3847 3006 AIAA JOURNAL, VOL. 51, NO. 12: 2013 INDEX J13-059 Mixofi Holnlowg-Con e Spray wiat Conhfin ed Crossflowi n J13-073 Differentia\ Interferometric Measurement of Instability in a Rectangular Duct. Haibin Zhang, Bofeng Bai, Li Liu, Huijuan Sun, and Hypervelocity Boundary Layer. N. J. Parziale, J. E. Shepherd, and H. G. Junjie Yan, State Key Laboratory of Multiphase Flow in Power Engineering, Hornung, California Institute of Technology (51, 3, p. 750) Note Xi'an Jiaotong University, People’s Republic of China (51, 3, p. 615) Full Paper J13-074 Acoustic Control of Vortex-Induced Vibrations of a Tethered Sphere. R. van Hout, A. Katz, and D. Greenblatt, Technion—Israel J13-060 Momentum Coefficient as a Parameter for Aerodynamic Institute of Technology, Israel (51, 3, p. 754) Note Flow Control with Synthetic Jets. Sebastian D. Goodfellow, University of Toronto, Canada; Serhiy Yarusevych, University of Waterloo, Canada; and J13-075 Control of Buffet Phenomenon on a Transonic Swept Wing. Pierre E. Sullivan, University of Toronto, Canada (51, 3, p. 623) Full Paper P. Molton, J. Dandois, A. Lepage, V. Brunet, and R. Bur, ONERA-The French Aerospace Lab, France (51, 4, p. 761) Full Paper based on AIAA Paper 2010- J13-061 Acoustic Velocity Formulation for Sources in Arbitrary 5494 Motion. G. Ghorbaniasl, Vrije Universiteit Brussel, Beigium; M. Carley, University of Bath, United Kingdom; and C. Lacor, Vrije Universiteit Brussel, J13-076 Large-Eddy Simulation of an Oscillating Cylinder in a Belgium (51, 3, p. 632) Full Paper Steady Flow. A. Feymark, Chalmers University of Technology, Sweden; N. Alin, Swedish Defense Research Agency, Sweden; R. E. Bensow, Chalmers J13-062 Adaptive Hybrid Surrogate Modeling for Complex University of Technology, Sweden; and C. Fureby, Swedish Defense Research Systems. Jie Zhang, Souma Chowdhury, and Jungiang Zhang, Rensselaer Agency, Sweden (51, 4, p. 773) Full Paper based on AIAA Paper 2010-560 Polytechnic Institute, Achille Messac, Syracuse University, and Luciano Castillo, Texas Tech University (51, 3, p. 643) Full Paper J13-077 Kinetic Node-Pair Formulation for Two-Dimensional Flows from Continuum to Transitional Regime. M. Fossati, McGill University, J13-063 Geometric Optimization of a Cylindrical Plasma Adaptive Canada; A. Guardone and L. Vigevano, Politecnico di Milano, Italy; and Optics Lens. Brian W. Neiswander, Eric Matlis, and Thomas C. Corke, K. Xu, Hong Kong University of Science and Technology, People’s Republic University of Notre Dame (51, 3, p. 657) Full Paper based on AIAA Paper of China (51, 4, p. 784) Full Paper 2012-0625 J13-064 Broadband Shock-Associated Noise in Screeching and Non- J13-078 Comparison of Adaptive Sampling Methods for Generation Screeching Underexpanded Supersonic Jets. Benoit André, Thomas of Surrogate Aerodynamic Models. T. J. Mackman and C. B. Allen, Castelain, and Christophe Bailly, Ecole Centrale de Lyon, France (51, 3, University of Bristol, United Kingdom; M. Ghoreyshi, U.S. Air Force p. 665) Full Paper Academy, and K. J. Badcock, University of Liverpool, United Kingdom (51, 4, p. 797) Full Paper based on AIAA Paper 2011-1171 J13-065 Application of the Scale-Adaptive Simulation to a Hot Jet in Cross Flow. Benjamin M. Duda, Airbus Operations SAS, France; Florian R. J13-079 High Frequency Pulsed Injection into a Supersonic Duct Menter, ANSYS Germany GmbH, Germany; Sébastien Deck, ONERA-The Flow. A. D. Cutler and G. C. Harding, George Washington University; and French Aerospace Laboratory, France, Hervé Bézard, ONERA-The French G. S. Diskin, NASA Langley Research Center (51, 4, p. 809) Full Paper based Aerospace Laboratory, France; Thorsten Hansen, ANSYS Germany GmbH, on AIAA Paper 2001-517 Germany; and Marie-Josephe Estéve, Airbus Operations SAS, France (51, 3, p. 674) Full Paper J13-080 Use of Sweeping Jets During Transient Deployment of a Control Surface. Elisa Phillips and Israel Wygnanski, University of Arizona J13-066 Vibrations of an Axially Moving Beam with Deployment or (51, 4, p. 819) Full Paper based on AIAA Paper 2010-4246 Retraction. Sungpil Park, Hanyang University, Republic of Korea; Hong Hee Yoo, Hanyang University, Republic of Korea; and Jintai Chung, Hanyang J13-081 Density Measurements of a Turbulent Wake Using Acetone University, Republic of Korea (51, 3, p. 686) Full Paper Planar Laser-Induced Fluorescence. John Z. Reid, Kyle P. Lynch, and Brian S. Thurow, Auburn University (51, 4, p. 829) Full Paper based on AIAA Paper J13-067 Zonal Detached Eddy Simulation of a Civil Aircraft with a 2011-0987 Deflected Spoiler. F.Gand, ONERA—The French Aerospace Lab, France (51, 3, p. 697) Full Paper J13-082 Thermal Shock Resistance of Ultra-High-Temperature Ceramics Under Aerodynamic Thermal Environments. Tianbao Cheng, J13-068 Efficient Mesh Deformation Using Radial Basis Functions Chongqing University, People’s Republic of China; Weiguo Li, State Key on Unstructured Meshes. Chunhua Sheng, University of Toledo; and Laboratory of Coal Mine Disaster Dynamics and Control, Chongging Christian B. Allen, University of Bristol, U.K. (51, 3, p. 707) Full Paper based University, People’s Republic of China; and Daining Fang, State Key on AIAA Paper 2012-2685 Laboratory for Turbulence and Complex Systems, Peking University, People’s Republic of China (51, 4, p. 840) Full Paper J13-069 Noise Predictions for Rectangular Jets Using a Conformal Mapping Method. S. J. Leib, Ohio Aerospace Institute (51, 3, p. 721) Full J13-083 Modeling of Bombardment Ejections in the Rotorcraft Paper Brownout Problem. Monica Syal and J. Gordon Leishman, University of J13-070 Eigensensitivity Analysis for Asymmetric Nonviscous Maryland (51, 4, p. 849) Full Paper Systems. Li Li, Yujin Hu, Xuelin Wang, and Ling Ling, Huazhong University of Science and Technology, People’s Republic of China (51, 3, p. 738) Note J13-084 Fast Low-Storage Method for Evaluating Lighthill’s Volume Quadrupoles. P. Croaker, N. Kessissoglou, and R. Kinns, University J13-071 Effect of the Initial Turbulence Level on anU nderexpanded of New South Wales, Australia; and S. Marburg, Bundeswehr University Supersonic Jet. J. Liu, K. Kailasanath, and J. P. Boris, Naval Research Munich, Germany (51, 4, p. 867) Full Paper Laboratory, and N. Heeb, D. Munday, and E. Gutmark, University of Cincinnati (51, 3, p. 741) Note J13-085 Energy-Release Rate and Mode Mixity of Face/Core Debonds in Sandwich Beams. George A. Kardomateas, Georgia Institute of J13-072 Application of Collaborative Optimization to Optimal Technology; Christian Berggreen, Technical University of Denmark, Denmark Control Problems. Xiang Li, Beijing Institute of Technology, People’s ; and Leif A. Carlsson, Florida Atlantic University (51, 4, p. 885) Full Paper Republic of China; ChangAn Liu, Xi'an Aerospace Propulsion Institute, Shaanxi Province, People’s Republic of China; Weiji Li, Northwestern J13-086 Detailed Computational Investigation of a Hovering Polytechnical University, Shaanxi Province, People’s Republic of China; and Microscale Rotor in Ground Effect. Vinod K. Lakshminarayan, Tarandeep Haibin Shang, Beijing Institute of Technology, People’s Republic of China S. Kalra, and James D. Baeder, University of Maryland (51, 4, p. 893) Full (51, 3, p. 745) Note Paper based on AIAA Paper 2011-3552 AIAA JOURNAL, VOL. 51, NO. 12: 2013 INDEX 3007 J13-087 Reduced-Order Dynamic Stall Modeling with Swept Flow J13-101 Leading-Edge Flow Structure of a Dynamically Pitching Effects Using a Surrogate-Based Recurrence Framework. Bryan Glaz, NACA 0012 Airfoil. B. J. Pruski and R. D. W. Bowersox, Texas A&M U.S. Army Research Laboratory; Peretz P. Friedmann and Li Liu, University of University (51, 5, p. 1042) Full Paper based on AIAA Paper 2011-3257 Michigan; and Juan G. Cajigas, Jeremy Bain, and Lakshmi N. Sankar, Georgia Institute of Technology (51, 4, p. 910) Full Paper J13-102 Surface Potential and Electric Field Measurements in Plasma Actuators at Low Pressure. Timothy G. Nichols and Joshua L. J13-088 Correlation Between Emission, Electric, and Flow Proper- Rovey, Missouri University of Science and Technology (51, 5, p. 1054) Full ties of Arc-Filament Plasma Actuators. Bradley DeBlauw, Bradley Sanders, Paper based on AIAA Paper Nick Glumac, Craig Dutton, and Gregory Elliott, University of Illinois at Urbana-Champaign (51, 4, p. 922) Full Paper based on AIAA Paper 2012- J13-103 Embedded Large-Eddy Simulation Using the Partially 190 Averaged Navier-Stokes Model. Lars Davidson, Chalmers University of Technology, Sweden; and Shia-Hui Peng, FOI, Swedish Defence Research J13-089 Strength Prediction in Open Hole Composite Laminates by Agency, Sweden (51, 5, p. 1066) Full Paper based on AIAA Paper 2011-3108 Using Discrete Damage Modeling. Michael J. Swindeman, Ende! V. Iarve, and Robert A. Brockman, University of Dayton Research Institute; David H. J13-104 Particle-Clustering Algorithms for the Prediction of Mollenhauer, U.S. Air Force Research Laboratory; and Stephen R. Hallett, Brownout Dust Clouds. Bharath Govindarajan, J. Gordon Leishman, and University of Bristol, United Kingdom (51, 4, p. 936) Full Paper based on Nail A. Gumerov, University of Maryland (51, 5, p. 1080) Full Paper AIAA Paper 2011-1793 J13-105 Stabilization of Explicit Fiow Solvers Using a Proper- J13-090 Multiparameter Analysis of Aero-Icing Problems Using Orthogonal-Decomposition Technique. Kivanc Ekici, University of Proper Orthogonal Decomposition and Multidimensional Interpolation. Tennessee, Kenneth C. Hall, Duke University; Huang Huang, University of Marco Fossati and Wagdi G. Habashi, McGill University, Canada (51, 4, Tennessee, and Jeffrey P. Thomas, Duke University (51, 5, p. 1095) Full Paper p. 946) Full Paper based on AIAA Paper 2012-1096 J13-091 Closed-Loop Performance Control of Dielectric-Barrier- J13-106 Aerodynamic Interactions of Reaction-Control-System Jets Discharge Plasma Actuators. Jochen Kriegseis, Daniel Schréter, Katrin for Atmospheric Entry Aeroshells. Hicham Alkandry and Iain D. Boyd, Barckmann, Alexander Duchmann, Cameron Tropea, and Sven Grundmann, University of Michigan; and Erin M. Reed, Joshua R. Codoni, and James C. Technische Universitit Darmstadt, Germany (51, 4, p. 961) Full Paper based on AIAA Paper 2012-2803 McDaniel, University of Virginia (51, 5, p. 1105) Full Paper based on AIAA Paper 2012-1013 J13-092 Investigation of High-Lift Mechanisms for a Flat-Plate Airfoil Undergoing Small-Amplitude Plunging Oscillations. D. J. Cleaver, J13-107 Statistical Vortex-Generator-Jet Model for Turbulent Flow Z. Wang, and I. Gursul, University of Bath, United Kingdom (51, 4, p. 968) Separation Control. Florian von Stillfried, Stefan Wallin, and Ame V. Full Paper based on AIAA Paper 2012-756 Johansson, Royal Institute of Technology, Sweden (51, 5, p. 1119) Full Paper J13-093 Large-Eddy Simulation of Natural Low-Frequency J13-108 Closed-Loop Dynamic Stall Control Using a Plasma Oscillations of Separating—Reattaching Flow Near Stall Conditions. Actuator. Andrew J. Lombardi, Patrick O. Bowles, and Thomas C. Corke, Jaber H. Almutairi, College of Technological Studies, Kuwait; and Ibraheem University of Notre Dame (51, 5, p. 1130) Full Paper based on AIAA Paper M. AlQadi, King Abdulaziz University, Saudi Arabia (51, 4, p. 981) Full Paper 2012-918 based on AIAA Paper 2012-2698 J13-109 Intermittent Nature of Subsonic Jet Noise. M. Kearney- J13-094 Multidimensional Numerical Noise from Captured Shock Fischer, A. Sinha, and M. Samimy, Ohio State University (51, 5, p. 1142) Full Wave and Its Cure. Eiji Shima and Keiichi Kitamura, Japan Aerospace Paper based on AIAA Paper 2012-1167 Exploration Agency, Japan (51, 4, p. 992) Note based on AIAA Paper 2009- 3544 J13-110 Improved Matrix Fraction Approximation of Aerodynamic Transfer Matrices. M. Ripepi and P. Mantegazza, Politecnico di Milano, Italy J13-095 Estimation of the Rheological Properties of a Suspension in (51, 5, p. 1156) Full Paper a Gel Fluid. Victor Chernov and Benveniste Natan, Technion—I/srael Institute of Technology, Israel (51, 4, p. 998) Note based on AIAA Paper 2010-6820 J13-111 Subgrid-Scale Models for Large-Eddy Simulations of Shock-Boundary-Layer Interactions. Avinash Jammalamadaka, Zhaorui J13-096 Quasi-Static Shape Control of Flexibie Space Structures by Li, and Farhad A. Jaberi, Michigan State University (51, 5, p. 1174) Full Paper Using Heaters. Junhui Zhang, Zhihai Xiang, and Yinghua Liu, Tsinghua University, People’s Republic of China (51, 4, p. 1003) Note J13-112 Rotating Beams Isospectral to Axially Loaded Nonrotating Uniform Beams. Sandilya Kambampati, Ranjan Ganguli, and V. Mani, /ndian J13-097 Evaluation of Laser Beacon for Adaptive-Optic Correction Institute of Science, India (51, 5, p. 1189) Full Paper of aC ompressible Shear Layer. R. Mark Rennie, University of Notre Dame; David Goorskey and Matthew R. Whiteley, MZA Associates Corporation; and J13-113 Stabilization of a Hypersonic Boundary Layer Using a David Cavalieri and Eric J. Jumper, University of Notre Dame (51, 4, p. 1008) Wavy Surface. Dmitry Bountin, Timur Chimitov, and Anatoly Maslov, Note based on AIAA Paper 2010-4494 Institute of Theoretical and Applied Mechanics, Russia; Andrey Novikov, and Ivan Egorov, Central Aerohydrodynamic Institute (TsAGI), Russia; Alexander J13-098 Compressive Sensing and Reconstruction in Measurements Fedorov, Moscow Institute of Physics and Technology, Russia; and Sergey with an Aerospace Application. Xun Huang, Peking University, People’s Utyuzhnikov, University of Manchester, United Kingdom (51,5, p. 1203) Full Republic of China (51, 4, p. 1011) Note Paper based on AIAA Paper J13-099 Robustness-Based Design Optimization of Multidiscipli- nary System Under Epistemic Uncertainty. Kais Zaman, Bangladesh J13-114 Energy-Vorticity Turbulence Model with Application to University of Engineering & Technology, Bangladesh; and Sankaran Flow Near Rough Surfaces. W. F. Phillips, E. B. Fowler, and D. F. Hunsaker, Mahadevan, Vanderbilt University (51, 5, p. 1021) Full Paper Utah State University (51, 5, p. 1211) Full Paper based on AIAA Paper J13-100 Active Control of Flow Separation on a Laminar Airfoil. J13-115 Shock Wave/Boundary-Layer Interaction Control Using a Nathan O. Packard, Michael P. Thake, Carlos H. Bonilla, Kyle Gompertz, and Combination of Vortex Generators and Bleed. Neil Titchener and Holger Jeffrey P. Bons, Ohio State University (51, 5, p. 1032) Full Paper based on Babinsky, University of Cambridge, United Kingdom (51, 5, p. 1221) Full AIAA Paper 2010-4579 Paper based on AIAA Paper 2012-274 3008 AIAA JOURNAL, VOL. 51, NO. 12: 2013 INDEX J13-116 Effects of Porous Walls on Hypersonic Boundary Layers J13-131 Three-Dimensional Stabilized Finite Elements for Com- over a Sharp Cone. Sharon O. Stephen and Vipin Michael, University of pressible Navier-Stokes. J. Taylor Erwin, W. Kyle Anderson, Sagar Kapadia, Birmingham, United Kingdom (51, 5, p. 1234) Full Paper based on AIAA and Li Wang, University of Tennessee at Chattanooga (51, 6, p. 1404) Full Paper 2010-4286 Paper based on AIAA Paper 2011-3411 J13-117 Decoupled Implicit Method for Aerothermodynamics and J13-132 Lift and Lift-Induced Drag Computation by Lamb Vector Reacting Flows. Graham V. Candler, Pramod K. Subbareddy, and loannis Integration. Claudio Marongiu, C/RA, Italian Aerospace Research Centre, Nompelis, University of Minnesota (51, 5, p. 1245) Full Paper based on AIAA Italy; Renato Tognaccini, University of Naples Federico II, \taly; and Makoto Paper 2012-5917 Ueno, Japan Aerospace Exploration Agency, Japan (51, 6, p. 1420) Full Paper J13-118 Classical, Refined, and Component-Wise Analysis of J13-133 Simultaneous Topology Optimization of Membrane Wings Reinforced-Shell Wing Structures. E. Carrera, A. Pagani, and M. Petrolo, and Their Compliant Flapping Mechanisms. Bret Stanford and Philip Politecnico di Torino, Italy (51, 5, p. 1255) Full Paper Beran, U.S. Air Force Research Laboratory, and Marcelo Kobayashi, University of Hawaii at Manoa (51, 6, p. 1431) Full Paper based on AIAA Ji3-11¢ Analysis of Numerical Errors Generated by Slowly Moving Paper 2012-1357 Shock Waves. Eric Johnsen, University of Michigan (51, 5, p. 1269) Note based on AIAA Paper J13-134 Buckling Optimization of Variable-Angle-Tow Panels Using the Infinite-Strip Method. Wenli Liu and Richard Butler, University J13-120 Resonant Frequency Determination of a Multistore High- of Bath, United Kingdom (51, 6, p. 1442) Full Paper based on AIAA Paper Altitude/Long-Endurance Wing. Adam D. Grasch, University of Bristol, 2012-1460 United Kingdom; Justin W. Jaworski, U.S. Air Force Research Laboratory; and Deman Tang and Earl H. Dowell, Duke University (51, 6, p. 1277) Full J13-135 Efficient Hybrid Surface/Volume Mesh Generation Using Paper Suppressed Marching-Direction Method. Yasushi Ito, University of Alabama at Birmingham; Mitsuhiro Murayama and Kazuomi Yamamoto, Japan Aerospace Exploration Agency, Japan; and Alan M. Shih and Bharat K. Ji3-121 Robust Design of a Reentry Unmanned Space Vehicle by Multifidelity Evolution Control. Edmondo Minisci and Massimiliano Soni, University of Alabama at Birmingham (51, 6, p. 1450) Full Paper based Vasile, University of Strathclyde, United Kingdom (51, 6, p. 1284) Full Paper on AIAA Paper 2011-3539 J13-136 Flow Control on a Thick Airfoil Using Suction Compared to J13-122 Nonparametric Stochastic Modeling of Structures with Blowing. Chunmei Chen, University of Arizona; Roman Seele, California Uncertain Boundary Conditions/Coupling Between Substructures. Marc Institute of Technology, and Israel Wygnanski, University of Arizona (51, 6, P. Mignolet, Arizona State University, Christian Soize, Université Paris-Est, p. 1462) Full Paper France; and Javier Avalos, Instituto Technolégico y de Estudios Superiores de Occidente (ITESO), Mexico (51, 6, p. 1296) Full Paper based on AIAA Paper J13-137 Transient Loads Occurring over a Thin Airfoil Subjected to Large-Scale Freestream Turbulence. Sridhar Ravi, University of Tubingen, J13-123 Generalization of the Far-Field Drag Decomposition Germany; and Simon Watkins, Jon Watmuff, and Alex Fisher, RMIT Method to Unsteady Flows. Martin Gariepy, Jean-Yves Trepanier, and University, Australia (51, 6, p. 1473) Full Paper Benoit Malouin, Ecole Polytechnique de Montréal, Canada (51, 6, p. 1309) Full Paper based on AIAA Paper 2011-3519 J13-138 Investigations of Azimuthal and Flight Effects on Noise from Realistic Turbofan Exhaust Geometries. K. Viswanathan and I. C. J13-124 Fuzzy Meshless Local Petrov-Galerkin Method for Analysis Lee, The Boeing Company (51, 6, p. 1486) Full Paper based on AIAA Paper of Imprecisely Defined Systems. Singiresu S. Rao and Jun Tian, University of Miami (51, 6, p. 1320) Full Paper J13-139 Separation Control by External Acoustic Excitation at Low Reynolds Numbers. S. L. Yang and G. R. Spedding, University of Southern J13-125 Data-Driven Model Development for the SuperSonic California (51, 6, p. 1506) Full Paper SemiSpan Transport. Sunil L. Kukreja, NASA Dryden Flight Research Center (51, 6, p. 1333) Full Paper based on AIAA Paper J13-140 Stability Enhanced High-Order Hyperviscosity-Based Shock Capturing Algorithm. Upender K. Kaul, NASA Ames Research J13-126 Multimodality and Global Optimization in Aerodynamic Center (51, 6, p. 1516) Note based on AIAA Paper 2011-3685 Design. Oleg Chernukhin and David W. Zingg, University of Toronto, Canada (51, 6, p. 1342) Full Paper based on AIAA Paper 2011-3070 J13-141 Experiments of Vortex-Induced Torsional Oscillation of a Flat Plate in Cross Flow. Yi Yang and Thomas W. Strganac, Texas A&M J13-127 Discrete Adjoint-Based Design for Unsteady Turbulent University (51, 6, p. 1522) Note based on AIAA Paper Flows on Dynamic Overset Unstructured Grids. Eric J. Nielsen, NASA Langley Research Center, and Boris Diskin, National Institute of Aerospace J13-142 Vibration Analysis of an Inflatable Torus Based on Mode (51, 6, p. 1355) Full Paper based on AIAA Paper 2012-0554 Shape. S. C. Gajbhiye, S. H. Upadhyay, and S. P. Harsha, Indian Institute of Technology Roorkee, India (51, 6, p. 1526) Note J13-128 Compact Implementation Strategy for a Harmonic Balance Method Within Implicit Flow Solvers. Jeffrey P. Thomas, Chad H. Custer, J13-143 Aero-Optic Effects of a Wingtip Vortex. Chris Porter, Mark Earl H. Dowell, and Kenneth C. Hall, Duke University; and Christophe Corre, Rennie and Eric Jumper, University of Notre Dame (51,7, p. 1533) Full Paper LEGI, Domaine Universitaire BP53, France (51, 6, p. 1374) Full Paper based based on AIAA Paper 2010-435 on AIAA Paper 2009-4270 J13-144 Coupled Airfoil Heave/Pitch Oscillations at Buffet Flow. J13-129 New Actuator-Disk Model for a Skewed Flow. Sivan Axel Hartmann, Michael Klaas, and Wolfgang Schréder, RWTH Aachen Kominer and Aviv Rosen, Technion—Israel Institute of Technology, Israel (51, University, Germany (51, 7, p. 1542) Full Paper based on AIAA Paper 2011- 6, p. 1382) Full Paper 3024 Ji3-130 Flight Measurements of the Aero-Optical Environment J13-145 Numerical Investigation of Passive Separation Control for Around a Flat-Windowed Turret. Chris Porter, Stanislav Gordeyev, Mike an Airfoil at Low-Reynolds-Number Conditions. A. Gross and H. F. Fasel, Zenk, and Eric Jumper, University of Notre Dame (51, 6, p. 1394) Full Paper University of Arizona (51, 7, p. 1553) Full Paper based on AIAA Paper 201 1- based on AIAA Paper 2011-3280 3439 AIAA JOURNAL, VOL. 51, NO. 12: 2013 INDEX 3009 J13-146 Numerical Analysis of a Scramjet Engine with Intake J1i3-160 Interpretation of Adjoint Solutions for Turbomachinery Sidewalls and Cavity Flameholder. Hyo-Won Yeom, Bong-Gyun Seo, and Flows. Andre C. Marta, Jnstituto Superior Técnico, Portugal; Sriram Hong-Gye Sung, Korea Aerospace University, Republic of Korea (51, 7, Shankaran, General Electric; Qigi Wang, Massachusetts Institute of p. 1566) Full Paper based on AIAA Paper 2011-5831 Technology; and Prem Venugopal, General Electric (51,7, p. 1733) Full Paper J13-147 Effect of Rotor Shielding on Fan-Outlet Guide Vanes J13-161 Solution of the Lossy Nonlinear Tricomi Equation Applied Broadband Noise Prediction. Héléne Posson, University of Cambridge, to Sonic Boom Focusing. Joseph A. Salamone and Victor W. Sparrow, United Kingdom; and Stéphane Moreau, Université de Sherbrooke, Canada Pennsylvania State University, and Kenneth J. Plotkin, Wyle (51, 7, p. 1745) (51, 7, p. 1576) Full Paper based on AIAA Paper 201 1-2878 Full Paper based on AIAA Paper 2013-935 J13-162 Hypersonic Test Analysis by Means of Aerothermal J13-148 Simulation of Tonal Noise Generation by Supersonic Coupling Methodology and Infrared Thermography. Marco Di Clemente Impinging Jets. Ali Uzun, Rajan Kumar, M. Yousuff Hussaini, and Farrukh S. and Giuseppe Rufolo, /talian Aerospace Research Centre; and Andrea Ianiro Alvi, Florida Center for Advanced Aero-Propulsion, Florida State University and Gennaro Cardone, University of Naples “Federico Il,”, Italy (51, 7, (51, 7, p. 1593) Full Paper p. 1755) Full Paper based on AIAA Paper 2009-7236 J13-149 Effect of Wing Twisting on Aerodynamic Performance of J13-163 Sound Generated by Boundary-Layer Flow over Small Flapping Wing System. Tri Quang Truong, Vu Hoang Phan, and Hoon Cheol Steps: Effect of Step Noncompactness. Jin Hao, Ahmed Eltaweel, and Meng Park, Konkuk University, Republic of Korea; and Jin Hwan Ko, Korea Institute Wang, University of Notre Dame (51, 7, p. 1770) Note based on AIAA Paper of Ocean Science & Technology, Republic of Korea (51, 7, p. 1612) Full Paper 2012-2051 J13-150 Flameholding in Converging and Turning Channels over J13-164 Induced-Drag Calculations in the Unsteady Vortex Lattice Cavities with Periodic Port Injection. Ben J. Colcord, William A. Sirignano, Method. Robert J. S. Simpson and Rafael Palacios, Imperial College London, and Feng Liu, University of California (51, 7, p. 1621) Full Paper United Kingdom; and Joseba Murua, University of Surrey, United Kingdom (51, 7, p. 1775) Note J13-151 Effect of Aspect Ratio on Aerodynamic Characteristics at J13-165 Reduction of Temperature Effects in Pressure-Sensitive Low Reynolds Numbers. Makoto Mizoguchi and Hajime Itoh, National Paint Measurements. Y. Egami, K. Fujii, and T. Takagi, Aichi Institute of Defense Academy, Japan (51, 7, p. 1631) Full Paper based on AIAA Paper Technology, Japan; and Y. Matsuda, H. Yamaguchi, and T. Niimi, Nagoya 2012-52 University, Japan (51, 7, p. 1779) Note based on AIAA Paper 2012-2759 J13-152 Fluid-Structure Interaction Simulations of a Tension-Cone J13-166 Iodine Tagging Velocimetry in a Mach 10 Wake. R. Jeffrey Inflatable Aerodynamic Decelerator. R. M. J. Kramer, University of Illinois Balla, NASA Langley Research Center (51, 7, p. 1783) Note at Urbana—Champaign; F. Cirak, University of Cambridge, United Kingdom; and C, Pantano, University of Illinois at Urbana—Champaign (51, 7, p. 1640) J13-167 Plasma Control of a Turbulent Shock Boundary-Layer Full Paper Interaction. Nicholas J. Bisek, Donald P. Rizzetta, and Jonathan Poggie, U.S. Air Force Research Laboratory (51, 8, p. 1789) Full Paper based on AIAA J13-153 Interaction of Three-Dimensional Protuberances with a Paper 2012-2700 Supersonic Turbulent Boundary Layer. Philip V. Hahn, NASA Marshall Space Flight Center, and Abdelkader Frendi, University of Alabama in J13-168 Spatially Developing Supersonic Turbulent Boundary Huntsville (51, 7, p. 1657) Full Paper based on AIAA Paper 2012-2172 Layer with a Body-Force-Based Method. Nathan J. Mullenix and Datta V. Gaitonde, Ohio State University; and Miguel R. Visbal, U.S. Air Force Research Laboratory (51, 8, p. 1805) Full Paper based on AIAA Paper J13-154 Slat Noise Assessment from Airbus A340 Flyover Phased- Array Microphone Measurements. V. Fleury and P. Malbéqui, OVERA— J13-169 Sidewall Boundary Layer of Transverse Waves in The French Aerospace Lab, France (51, 7, p. 1667) Full Paper Simulated Liquid Rocket Engines. Charles T. Haddad and Joseph Majdalani, University of Tennessee Space Institute (51, 8, p. 1820) Full Paper J13-155 A General Theory of Flow-Instability Inception in based on AJAA Paper 2012-4086 Turbomachinery. Xiaofeng Sun and Xiaohua Liu, Beihang University, People’s Republic of China; Ruiwei Hou, Shenyang Aeroengine Research J13-170 Vortex Dynamics in Transitional and Turbulent Boundary Institute, People’s Republic of China; and Dakun Sun, Beihang University, Layers. Peter S. Bernard, University of Maryland (51, 8, p. 1828) Full Paper People’s Republic of China (51, 7, p. 1675) Full Paper based on AIAA Paper based on AIAA Paper J13-156 *Geometric’ Viscous Damping Model for Nearly Constant J13-171 Open-Loop Flow-Control Investigation for Airfoils at Low Beam Modal Damping. George A. Lesieutre, Pennsylvania State University; Reynolds Numbers. C. Brehm, A. Gross, and H. F. Fasel, University of and Jeffrey L. Kauffman, University of Central Florida (51, 7, p. 1688) Full Arizona (51, 8, p. 1843) Full Paper based on AIAA Paper Paper based on AIAA Paper 2012-1873 J13-172 New Nonpolynomial Shear-Deformation Theories for Structural Behavior of Laminated-Composite and Sandwich Plates. J13-157 Suppression of Tonal Trailing-Edge Noise From an Airfoil Neeraj Grover, B. N. Singh, and D. K. Maiti, Indian Institute of Technology, Using a Plasma Actuator. Ayumu Inasawa, Chiho Ninomiya, and Masahito India (51, 8, p. 1861) Full Paper Asai, Tokyo Metropolitan University, Japan (51, 7, p. 1695) Full Paper J13-173 Conservative Formulation of the k-e Turbulence Model for J13-158 Inviscid Analysis of Extended-Formation Flight. James E. Shock-Turbulence Interaction. Krishnendu Sinha and S. J. Balasridhar, Kless, Science and Technology Corporation; Michael J. Aftosmis, NASA Indian Institute of Technology Bombay, India (51, 8, p. 1872) Full Paper Ames Research Center; S. Andrew Ning, Stanford University, Stanford; and Marian Nemec, Science and Technology Corporation (51, 7, p. 1703) Full J13-174 Simulation of Rapidly Maneuvering Airfoils with Synthetic Paper Jet Actuators. SolKeun Jee, NASA Ames Research Center, Omar D. Lopez Mejia, University of the Andes, Colombia; Robert D. Moser, University of J13-159 Simulations of Pitch-Heave Limit-Cycle Oscillations at a Texas at Austin; Jonathan A. Muse, U.S. Air Force Research Laboratory; Ali Transitional Reynolds Number. Weixing Yuan, National Research Council T. Kutay, Middle East Technical University, Turkey; and Anthony J. Calise, Canada, Canada; and Dominique Poirel and Baoyuan Wang, Royal Military Georgia Institute of Technology (51, 8, p. 1883) Full Paper based on AIAA College of Canada, Canada (51, 7, p. 1716) Full Paper Paper 3010 AIAA JOURNAL, VOL. 51, NO. 12: 2013 INDEX J13-175 Topology-Optimized Design and Testing of a Pressure- J13-191 Multidisciplinary Design Optimization: A Survey of Driven Morphing-Aerofoil Trailing-Edge Structure. Srinivas Vasista and Architectures. Joaquim R. R. A. Martins, University of Michigan; and Liyong Tong, University of Sydney, Australia (51, 8, p. 1898) Full Paper based Andrew B. Lambe, University of Toronto, Canada (51, 9, p. 2049) Survey on AIAA Paper Paper J13-176 Folding, Stowage, and Deployment of Viscoelastic Tape J13-192 Improved Solution of Equations by Regularizing Ill- Springs. Kawai Kwok and Sergio Pellegrino, California Institute of Conditioned Coefficient Matrix for System Identification. Masayoshi Technology (51, 8, p. 1908) Full Paper based on AIAA Paper 2011-2022 Misawa, Shizuoka University, Japan; Takashi Sekiya, Koryo Engineering Company, Japan; and Masaki Oba, Mitsubishi Electric Engineering Company, J13-177 Zonal Detached-Eddy Simulation of an Airfoil in Poststall Japan (51, 9, p. 2076) Full Paper Condition. A. Le Pape, F. Richez, and S. Deck, ONERA-The French Aerospace Lab, France (51, 8, p. 1919) Full Paper based on AIAA Paper 2012- J13-193 Dynamic Stall Control by Passive Disturbance Generators. 3287 Benjamin Heine and Karen Mulleners, DLR, German Aerospace Center, Germany; Gilles Joubert, ONERA-The French Aerospace Lab, France; and Ji13-178 Effects of Pulsation Intensity on Flow and Mixing of Markus Raffel, DLR, German Aerospace Center, Germany (51, 9, p. 2086) Swirling Double-Concentric Jets. S. R. Jufar, R. F. Huang, and C. M. Hsu, Full Paper based on AIAA Paper 2011-3371 National Taiwan University of Science and Technology, Republic of China (51, 8, p. 1932) Full Paper J13-194 Three-Component Laser-Doppler-Anemometry Measure- ments in Turbulent Swirling Jets. Richard Semaan and Jonathan W. J13-179 Nondomination-Level Coordinate System for Parameteriz- Naughton, University of Wyoming (51, 9, p. 2098) Full Paper based on AIAA ing and Exploring Pareto Frontiers. Matthew J. Daskilewicz and Brian J. Paper 2008-761 German, Georgia Institute of Technology (51, 8, p. 1946) Full Paper J13-195 Modified Linear-Membrane Formulation for the Pressur- J13-180 Aerodynamic Control of Low-Reynolds-Number Airfoil ized Torus and Multitorus. F. J. J. M. M. Geuskens, Delft University of with Leading-Edge Protuberances. M. M. Zhang, G. F. Wang, and J. Z. Xu, Technology, The Netherlands; J. T. Tielking, Texas A&M University; and S. Chinese Academy ofS ciences, People’s Republic of China (51, 8, p. 1960) Full Koussios and A. Beukers, Delft University of Technology, The Netherlands Paper (51, 9, p. 2114) Full Paper J13-181 Approach to Aerodynamic Design Through Numerical J13-196 Three-Dimensional Shock Wave Detection Based on the Optimization. Howard P. Buckley and David W. Zingg, University of Theory of Characteristics. Masashi Kanamori and Kojiro Suzuki, University Toronto, Canada (51, 8, p. 1972) Full Paper of Tokyo, Japan (51, 9, p. 2126) Full Paper based on AIAA Paper 2011-3681 J13-182 Study of Rotating Menisci in a Generic Propellant- J13-197 Biplane and Tail Effects in Flapping Flight. W. B. Tay, H. Management Device. Yvonne Reichel and Michael E. Dreyer, University of Bijl, and B. W. van Oudheusden, Delft University of Technology, The Bremen, Germany (51, 8, p. 1982) Full Paper based on AIAA Paper 201 1-6036 Netherlands (51, 9, p. 2133) Full Paper based on AIAA Paper J13-183 Geometrically Nonlinear Behavior of Sandwich Plates. Dvir J13-198 Hypersonic Turbulent Boundary-Layer Fuel Injection and Elmalich and Oded Rabinovitch, Technion—Israel Institute of Technology, Combustion: Skin-Friction Reduction Mechanisms. James E. Barth, Israel (51, 8, p. 1993) Full Paper Vincent Wheatley, and Michael K. Smart, University of Queensland, Australia (51, 9, p. 2147) Full Paper J13-184 Spreading Angle and Core Length Analysis of Supercritical Jets. Arnab Roy and Corin Segal, University of Florida; and Clément Joly, J13-199 Effectiveness of Spalart-Allmaras Turbulence Model in Centre National de la Recherche Scientifique ICARE, 45071 Orléans Cedex, Analysis of Curved Cooling Channels. Marco Pizzarelli, University of Rome France (51, 8, p. 2009) Full Paper “La Sapienza”, Italy (51, 9, p. 2158) Full Paper J13-185 Using Supervised Learning to Improve Monte Carlo J13-200 Effect of Spike Truncation on the Acoustic Behavior of Integral Estimation. Brendan Tracey, Stanford University, David Wolpert, Annular Aerospike Nozzles. N. Karthikeyan, Ashwin Kumar, S. B. Verma, Los Alamos National Laboratory, and Juan J. Alonso, Stanford University (51, and L. Venkatakrishnan, National Aerospace Laboratories, India (51, 9, 8, p. 2015) Full Paper based on AJAA Paper 2011-1843 p. 2168) Full Paper based on AIAA Paper 2009-3375 J13-186 Dynamic Characteristics Prediction of Large Structures by J13-201 Block Krylov Methods to Solve Adjoint Problems in Component Modal Tests. Masayoshi Misawa, Jyunichi Nakajima, and Aerodynamic Design Optimization. Xavier Pine! and Marc Montagnac, Hidenori Kawasoe, Shizuoka University, Japan (51, 8, p. 2024) Note Centre Européen de Recherche et de Formation Avancée en Calcul Scientifique, France (51, 9, p. 2183) Full Paper J13-187 Experimental Characterization of a Pulsed Plasma Jet. Todd M. Reedy, Nachiket V. Kale, J. Craig Dutton, and Gregory S. Elliott, J13-202 Output Feedback Control of Blasius Flow with Leading University of Illinois at Urbana-Champaign (51, 8, p. 2027) Note based on Edge Using Plasma Actuator. Reza Dadfar and Onofrio Semeraro, Royal AIAA Paper 2012-904 Institute of Technology, Sweden; Ardeshir Hanifi, Swedish Defence Research Agency (FOI), Sweden; and Dan S. Henningson, Royal Institute of J13-188 Tailoring Flapping Wings to Facilitate Desired Deformed Technology, Sweden (51, 9, p. 2192) Full Paper Shapes. Sameer Luthra, Zhiyuan Zhang, Raphael T. Haftka, and Ashok V. Kumar, University of Florida (51, 8, p. 2032) Note J13-203 Canonical Normal Shock Wave/Boundary-Layer Inter- action Flows Relevant to External Compression Inlets. Eric Loth, J13-189 Solution Characteristics of the Retarded-Time Equation for University of Virginia; Neil Titchener and Holger Babinsky, University of Transonic Rotating Sources. Honztao Tang, Yijun Mao, and Datong Qi, Cambridge, United Kingdom; and Louis Povinelli, NASA John H. Glenn Xi'an Jiaotong University, People’s Republic of China (51, 8, p. 2035) Note Research Center at Lewis Field (51, 9, p. 2208) Full Paper J13-190 Formation of Bifurcated Wakes Behind Finite Span J13-204 Thin-Wing Vibration Control Using Flexible Fins. Javier Flapping Wings. Meilin Yu and Z. J. Wang, University of Kansas; and Hui Montefort, Nicholas Pohl, and Tianshu Liu, Western Michigan University; Hu, lowa State University (51, 8, p. 2040) Note based on AIAA Paper 2012- James Gregory, Ohio State University; and Jim Crafton, Innovative Scientific 757 Solutions Inc. (51, 9, p. 2218) Full Paper