The Aeronautical Journal of the Royal Aeronautical Society INCORPORATING THE INSTITUTION OF AERONAUTICAL ENGINEERS, THE HELICOPTER ASSOCIATION OF GREAT BRITAIN AND THE SOCIETY OF LICENSED AIRCRAFT ENGINEERS AND TECHNOLOGISTS VOLUME XCVII JANUARY—DECEMBE19R9 3 SUBJECT INDEX AERODYNAMICS Kingsley, S. and Quegan, S. Understanding Radar Systems, p 179 (May). An aerodynamic model for flapping-wing flight, J.D. DeLaurier, pp 125-130 (Apr.). Knacke, T.W. Parachute Recovery Systems Design Manual, p 372 (Dec.). A summary of further measurements of steady and oscillatory pressures on Kuo, C. Business Fundamentals for Engineers, p 121 (Mar.). a rectangular wing, D.G. Mabey, B.L. Welsh and C.R. Pyne, pp 195-207 (Jun./Jul.). MacFadzean, R.H.M. Surface-Based Air Defence System Anaylsis, p 81 (Feb.) Experiments on a 60° delta wing with vortex flaps and vortex plates, K. Rinole, pp 33-38 (Jan.). Malyshev, V.V. et al Optimisation of Observation and Control Processes, p 81 (Feb.). Incompressible flow in contracting ducts, J.C. Gibbings, pp 230-246 (Aug./Sept.). Murthy, T.K.S. Computational Methods in Hypersonic Aerodynamics, p 260 (Aug./Sept.). The 33rd Lanchester Lecture. Automobile aerodynamics — the effects of airflow on road, racing and record breaking cars, J.L. Stollery, pp Murthy, S.N.B. and Curran, E.T. High-Speed Flight Propulsion Systems, 307-313 (Nov.). p 260 (Aug./Sept.). Wall jets created by single and twin high pressure jet impingement, Pnueli, D. and Gutfinger, G. Fluid Mechanics, p 298 (Oct.). P. Miller and M. Wilson, pp 87—100 (Mar.). Rogers, D.F. Laminar Flow Analysis, p 219 (Jun./Jul.). Technical Note: Optimisation of constant altitude—constant airspeed flight for piston prop aircraft, S.J. Ojha, pp 145-148 (Apr.) Simon, H.D. (Ed) Parallel Computation Fluid Dynamics: Implementations and Results, p 298 (Oct.). AEROFOILS Engineering Note: The use of colour graphics to show streamlines in Thornton, E.A. Thermal Structures and Materials for High Speed Flight, two-dimensional flow, S.J. Newman, pp 296-297 (Oct.). p 121 (Mar.). BOOK REVIEWS — BY AUTHOR Wendt, J.F. (Ed) Computational Fluid Dynamics — An Introduction, p 39 Blakelock, J.H. Automatic Control of Aircraft and Missiles — Second (Jan.). edition, p 39 (Jan.). Xu, Y. and Kanade, T. (Eds) Space Robotics, p 218 (Jun./Jul.). Bray, D.E. and McBride, D. (Eds), Nondestructive Testing Techniques, p 39 (Jan.). BOOK REVIEWS — BY TITLE Aerodynamics for Engineering Students — Fourth edition, E.L. Houghton Case, J. et al Strength of Materials and Structures: with an Introduction to and P.W. Carpenter, p 371 (Dec.). Finite Element Methods — Third edition, p 261 (Aug./Sept.) Analysis of Aircraft Structures: an Introduction, B.K. Donaldson, p 298 Chobotov, V. A. Spacecraft Attitude Dynamics and Control, p 121 (Mar.) (Oct.). Desrochers, A.A. (Ed) Intelligent Robotic Systems for Space Explo- Automatic Control of Aircraft and Missiles — Second edition, ration, p 179 (May). J.H. Blakelock, p 39 (Jan.). Donaldson, B.K. Anaylsis of Aircraft Structures: an Introduction, p 298 Business Fundamentals for Engineers, C. Kuo, p 121 (Mar.). (Oct.). Computational Fluid Dynamics — An Introduction, J.F. Wendt (Ed), p 39 Dimarogonas, A.D. and Haddad, S. Vibration for Engineers, p 150 (Apr.). (Jan.). Frashad, M. Design and Anaylsis of Shell Structures, p 218 (Jun./Jul.). Computational Methods in Hypersonic Aerodynamics, T.K.S Murthy, p 260 (Aug./Sept.). Gatski, T. et al (Eds) Studies of Turbulence: dedicated to John L. Lumley on the occasion of his sixtieth birthday, p 179 (May). Design and Analysis of Shell Structures, M. Frashad, p 218 (Jun./Jul.). Griffen, N.D. and French, J.R. Space Vehicle Design, p 149 (Apr.) Fluid Mechanics, D. Pnueli and G. Gutfinger, p 298 (Oct.). Hill, P. and Peterson, C. Mechanics and Thermodynamics of Propulsion High-Speed Flight Propulsion Systems, S.N.B. Murthy and E.T. Curran — Second edition, p 371 (Dec.). (Eds), p 260 (Aug./Sept.). Houghton, E.L. and Carpenter, P.W. Aerodynamics for Engineering Intelligent Robotic Systems for Space Exploration, A.A. Desrochers (Ed), Students — Fourth edition, p 371 (Dec.). p 179 (May). Subject index Aeronautical Journal December1993 The Aeronautical Journal of the Royal Aeronautical Society INCORPORATING THE INSTITUTION OF AERONAUTICAL ENGINEERS, THE HELICOPTER ASSOCIATION OF GREAT BRITAIN AND THE SOCIETY OF LICENSED AIRCRAFT ENGINEERS AND TECHNOLOGISTS VOLUME XCVII JANUARY—DECEMBE19R9 3 SUBJECT INDEX AERODYNAMICS Kingsley, S. and Quegan, S. Understanding Radar Systems, p 179 (May). An aerodynamic model for flapping-wing flight, J.D. DeLaurier, pp 125-130 (Apr.). Knacke, T.W. Parachute Recovery Systems Design Manual, p 372 (Dec.). A summary of further measurements of steady and oscillatory pressures on Kuo, C. Business Fundamentals for Engineers, p 121 (Mar.). a rectangular wing, D.G. Mabey, B.L. Welsh and C.R. Pyne, pp 195-207 (Jun./Jul.). MacFadzean, R.H.M. Surface-Based Air Defence System Anaylsis, p 81 (Feb.) Experiments on a 60° delta wing with vortex flaps and vortex plates, K. Rinole, pp 33-38 (Jan.). Malyshev, V.V. et al Optimisation of Observation and Control Processes, p 81 (Feb.). Incompressible flow in contracting ducts, J.C. Gibbings, pp 230-246 (Aug./Sept.). Murthy, T.K.S. Computational Methods in Hypersonic Aerodynamics, p 260 (Aug./Sept.). The 33rd Lanchester Lecture. Automobile aerodynamics — the effects of airflow on road, racing and record breaking cars, J.L. Stollery, pp Murthy, S.N.B. and Curran, E.T. High-Speed Flight Propulsion Systems, 307-313 (Nov.). p 260 (Aug./Sept.). Wall jets created by single and twin high pressure jet impingement, Pnueli, D. and Gutfinger, G. Fluid Mechanics, p 298 (Oct.). P. Miller and M. Wilson, pp 87—100 (Mar.). Rogers, D.F. Laminar Flow Analysis, p 219 (Jun./Jul.). Technical Note: Optimisation of constant altitude—constant airspeed flight for piston prop aircraft, S.J. Ojha, pp 145-148 (Apr.) Simon, H.D. (Ed) Parallel Computation Fluid Dynamics: Implementations and Results, p 298 (Oct.). AEROFOILS Engineering Note: The use of colour graphics to show streamlines in Thornton, E.A. Thermal Structures and Materials for High Speed Flight, two-dimensional flow, S.J. Newman, pp 296-297 (Oct.). p 121 (Mar.). BOOK REVIEWS — BY AUTHOR Wendt, J.F. (Ed) Computational Fluid Dynamics — An Introduction, p 39 Blakelock, J.H. Automatic Control of Aircraft and Missiles — Second (Jan.). edition, p 39 (Jan.). Xu, Y. and Kanade, T. (Eds) Space Robotics, p 218 (Jun./Jul.). Bray, D.E. and McBride, D. (Eds), Nondestructive Testing Techniques, p 39 (Jan.). BOOK REVIEWS — BY TITLE Aerodynamics for Engineering Students — Fourth edition, E.L. Houghton Case, J. et al Strength of Materials and Structures: with an Introduction to and P.W. Carpenter, p 371 (Dec.). Finite Element Methods — Third edition, p 261 (Aug./Sept.) Analysis of Aircraft Structures: an Introduction, B.K. Donaldson, p 298 Chobotov, V. A. Spacecraft Attitude Dynamics and Control, p 121 (Mar.) (Oct.). Desrochers, A.A. (Ed) Intelligent Robotic Systems for Space Explo- Automatic Control of Aircraft and Missiles — Second edition, ration, p 179 (May). J.H. Blakelock, p 39 (Jan.). Donaldson, B.K. Anaylsis of Aircraft Structures: an Introduction, p 298 Business Fundamentals for Engineers, C. Kuo, p 121 (Mar.). (Oct.). Computational Fluid Dynamics — An Introduction, J.F. Wendt (Ed), p 39 Dimarogonas, A.D. and Haddad, S. Vibration for Engineers, p 150 (Apr.). (Jan.). Frashad, M. Design and Anaylsis of Shell Structures, p 218 (Jun./Jul.). Computational Methods in Hypersonic Aerodynamics, T.K.S Murthy, p 260 (Aug./Sept.). Gatski, T. et al (Eds) Studies of Turbulence: dedicated to John L. Lumley on the occasion of his sixtieth birthday, p 179 (May). Design and Analysis of Shell Structures, M. Frashad, p 218 (Jun./Jul.). Griffen, N.D. and French, J.R. Space Vehicle Design, p 149 (Apr.) Fluid Mechanics, D. Pnueli and G. Gutfinger, p 298 (Oct.). Hill, P. and Peterson, C. Mechanics and Thermodynamics of Propulsion High-Speed Flight Propulsion Systems, S.N.B. Murthy and E.T. Curran — Second edition, p 371 (Dec.). (Eds), p 260 (Aug./Sept.). Houghton, E.L. and Carpenter, P.W. Aerodynamics for Engineering Intelligent Robotic Systems for Space Exploration, A.A. Desrochers (Ed), Students — Fourth edition, p 371 (Dec.). p 179 (May). Subject index Aeronautical Journal December1993 Laminar Flow Analysis, D.F. Rogers, p 219 (Jun./Jul.). CONTROL SYSTEMS Stability augmentation of a sailplane in towed flight, G. de Matteis and Mechanics and Thermodynamics of Propulsion — Second edition, P. Hill W. Tamilia, pp 349-358 (Dec.). and C. Peterson, p 371 (Dec.). DESIGN AND DEVELOPMENT Nondestructive Testing Techniques, D.E. Bray and D. McBride (Eds), An aerodynamic model for flapping-wing flight, J.D. DeLaurier, pp p 39 (Jan.). 125-130 (Apr.). Optimisation of Observation and Control Processes, V.V. Malyshev et al, A study of mechanical flapping-wing flight, J.D. DeLaurier and J.M. p 81 (Feb.). Harris, pp 277-286 (Oct.). Parachute Recovery Systems Design Manual, T.W. Knacke, p 372 (Dec.). Integration of high bypass ratio engines on modern transonic wings for re- gional aircraft, E. Greff, K. Becker, M. Karwin and S. Rill, pp 1-13 Parallel Computation Fluid Dynamics: Implementations and Results, H.D. (Jan.). Simon (Ed), p 298 (Oct.). Machinery arrangements for Vtol transport aircraft, D.C. MacPhail, A.S. Spacecraft Attitude Dynamics and Control, V. A. Chobotov, p 121 (Mar.). Jackson and E.S. Moore, pp 101—110, (Mar.). Space Robotics, Y. Xu and T. Kanade (Eds), p 218 (Jun./Jul.). The contributions of Power Jets Ltd to jet propulsion, G.B.R. Feilden, pp 62-72 (Feb.). Space Vehicle Design, N.D. Griffen and J.R. French, p 149 (Apr.). The development of an efficient ornithopter wing, J.D. DeLaurier, Strength of Materials and Structures: with an Introduction to Finite pp 153-162 (May). Element Methods — Third edition, J. Case et al, p 261 (Aug./Sept.). DRAG Studies of Turbulence: dedicated to John L. Lumley on the occasion of his Cavity drag at transonic speeds, L.C. Squire and S.H. Nasser, pp 247-256 sixtieth birthday, T. Gatski et al (Eds), p 179 (May). (Aug./Sept.). Surface-Based Air Defence System Anaylsis, R.H.M. MacFadzean, p 81 Technical Note: Optimisation of constant altitude—constant airspeed flight (Feb.). for piston prop aircraft, S.J. Ojha, pp 145-148 (Apr.) Thermal Structures and Materials for High Speed Flight, E.A. Thornton, ENGINE-AIRFRAME INTEGRATION p 121 (Mar.). Integration of high bypass ratio engines on modern transonic wings for re- Understanding Radar Systems, S. Kingsley and S. Quegan, p 179 (May). gional aircraft, E. Greff, K. Becker, M. Karwin and S. Rill, pp 1-13 (Jan.). Vibration for Engineers, A.D. Dimarogonas and S. Haddad, p 150 (Apr.). Machinery arrangements for Vtol transport aircraft, D.C. MacPhail, A.S. BOUNDARY LAYERS Jackson and E.S. Moore, pp 101—110 (Mar.). A pressure instrument to measure skin friction in turbulent boundary Technical Note: Optimisation of constant altitude—constant airspeed flight layers on smooth and non-smooth walls, P.V. Storm and _ B.G. for piston prop aircraft, S.J. Ojha, pp 145-148 (Apr.) Newman, pp 25-32 (Jan.). FINITE ELEMENTS An experimental study of the interaction of an unsteady shock with turbu- Stress concentration factors in countersunk holes, J.B. Young and lent boundary layer at Mach numbers of 1-3 and 1-5, J.A. Edwards K.K. Lee, pp 267-276 (Oct.). and L.C. Squire, pp 337-348 (Dec.). FLIGHT OPERATIONS Computational modelling of shock wave/boundary layer interaction with a An economic puzzle for airline management — how to recover mandatory cell-vertex scheme and transport models of _ turbulence, investments, J.M. Mariani, pp 368-370 (Dec.).- M.A. Leschziner, K.P. Dimitriadis and G. Page, pp 43-61 (Feb.). FLUID DYNAMICS: FLOW Transonic shockwave/turbulent boundary layer interactions on a porous A pressure instrument to measure skin friction in turbulent boundary surface, N. Chokani and L.C. Squire, pp 163—170 (May). layers on smooth and non-smooth walls, P.V. Storm and B.G. BUCKLING AND INSTABILITY OF STRUCTURES Newman, pp 25-32 (Jan.). Orthotropic behaviour of shells and stability of uniaxially compressed Erratum: A pressure instrument to measure skin friction in turbulent cylinders, M.S. Hanna and A.W. Beshara, pp 1 11—117 (Mar.). boundary layers on smooth and non-smooth walls, P.V. Storm and B.G. Newman, p 208 (Jun./Jul.). CANARDS An equation decoupling technique for identification of unstable aircraft Experimental study of overexpanded supersonic jet impingement on a with unsteady aerodynamic modelling, J. Singh and S.C. double wedge deflector, J.K. Prasad, R.C. Mehta and A.K. Seekanth, Raisinghani, pp 321-327 (Nov.). pp 209-214 (Jun./Jul.). COMPUTATIONAL FLUID DYNAMICS Further study of high speed single free jets, G.H. Moustafa, pp 171-176 An equation decoupling technique for identification of unstable aircraft (May). with unsteady aerodynamic modelling, J. Singh and _ S.C. Raisinghani, pp 321-327 (Nov.). Gas jets in an arbitrary stream, R.M.C. So and H. Aksoy, pp 287-295 (Oct.). A vortex lattice method for thin wings oscillating in ideal flow, M.K. Laha, pp 314-320 (Nov.). Incompressible flow in contracting ducts, J.C. Gibbings, pp 230-246 (Aug./Sept.). Computational modelling of shock wave/boundary layer interaction with a cell-vertex scheme and transport models of turbulence, Self adaptive mesh refinement for the computation of steady, compress- M.A. Leschziner, K.P. Dimitriadis and G. Page, pp 43-61 (Feb.). ible, viscous flows, J. Fischer, pp 357-368 (Dec.). Self adaptive mesh refinement for the computation of steady, compress- The solution of the Navier-Stokes equations for two-dimensional ible, viscous flows, J. Fischer, pp 357-368 (Dec.). compressible flows using a simple second order accurate algorithm, K.P. Sinhamahapatra, pp 131-137 (Apr.). The solution of the Navier-Stokes equations for two-dimensional compressible flows using a simple second order accurate algorithm, Wall jets created by single and twin high pressure jet impingement, K.P. Sinhamahapatra, pp 131—137 (Apr.). P. Miller and M. Wilson, pp 87—100 (Mar.). Aeronautical Journal December1993 Subject index Engineering Note: The use of colour graphics to show streamlines in two Meteor in flight, p 67 (Feb.). dimensional flow, S.J. Newman, pp 296-297 (Oct.). Tornado F.3s deployed to Dhahran within three days of go-ahead, p 224 (Aug./Sept.). FLUTTER Hercules wing tip damage after a ground collision with a Puma, p 225 A summary of further measurements of steady and oscillatory pressures on (Aug./Sept.). a rectangular wing, D.G. Mabey, B.L. Welsh and C.R. Pyne The same Hercules wing tip after a battle damage repair, p pp 195-207 (Jun./Jul.). (Aug./Sept.). An RAF deployment; a TriStar leads four Tornado F.3s, p A vortex lattice method for thin wings oscillating in ideal flow, (Aug./Sept.). M.K. Laha, pp 314-320 (Nov.). Automobiles An equation decoupling technique for identification of unstable aircraft The Gold Medal Phaeton, 1898, Lanchester driving his brother, George, with unsteady aerodynamic modelling, J. Singh and S.C. nearest the camera, p 307 (Nov.). Raisinghani, pp 321-327 (Nov.). Thrust II at Black Rock Desert, 1983, p 313 (Nov.). Stability augmentation of a sailplane in towed flight, G. de Matteis and W. Tamilia, pp 349-358 (Dec.). Engines First build of the Whittle WU engine, on test in the BTH works, Rugby, HEAT TRANSFER p 63 (Feb.). Technical Note: The use of a Flame Ionisation Detector for mass fraction Third build of experimental engine, on test at Ladywood Works, Lutter- measurement in short duration windtunnels, I.N.R. Bowman and worth, p 63 (Feb.). J.A. Edwards, pp 215-217 (Jun./Jul.). W1 flight engine on the stand at the Ladywood Works, p 64 (Feb.). Power jets W2/700 engine, p 68 (Feb.). HISTORICAL The Rolls-Royce Derwent V, p 68 (Feb.). The contributions of Power Jets Ltd to jet propulsion, G.B.R. Feilden, pp 62-72 (Feb.). Historical The Sir Sydney Camm legacy, p 223, (Aug./Sept.). HYPERSONICS Technical Note: The use of a Flame Ionisation Detector for mass fraction Large components measurement in short duration windtunnels, I.N.R. Bowman and Early combustion chamber test rig, p 64 (Feb.). J.A. Edwards, pp 215-217 (Jun./Jul.). Rotor of the Power Jets W2/700 engine, p 67 (Feb.). JETS Experimental study of overexpanded supersonic jet impingement on a Operations double wedge deflector, J.K. Prasad, R.C. Mehta and A.K. Seekanth, The sea ice airstrip at Cape Dyer, Baffin Island, p 102 (Mar.). pp 209-214 (Jun./Jul.). Winding road to airstrip, eastern Artic Canada, p 102 (Mar.). Icestrip operation, eastern Artic, p 102 (Mar.). Further study of high speed single free jets, G.H. Moustafa, pp 171-176 Break-up chaos at Hall Beach in July, p 102 (Mar.). (May). Logging scene, Mt Sir Francis Drake, Bute Inlet, British Columbia, p 103 (Mar.). Gas jets in an arbitrary stream, R.M.C. So and H. Aksoy, pp 287-295 (Oct.). Ornithopters “Tim Bird” rubber powered model ornithopter, p 277 (Oct.). Wall jets created by single and twin high pressure jet impingement, Ornithopter in flight, 4 September 1991, p 284 (Oct.). P. Miller and M. Wilson, pp 87—100, (Mar.). LOGISTICS Test results The 1ith Sir Sydney Camm Lecture. Supporting the Royal Air Force The forebody primary vortices in symmetric (@ = 20°) and asymmetric the challenge for Logistics Command approaching the 21st century, (a = 30°) conditions, p 78 (Feb.). R.J.M. Alcock, pp 223-229 (Aug./Sept.). The interaction of the strake vortex with the lifting surface (a = 10°) at x/1 = 0-66, p 79 (Feb.). NACELLES Interferogram of flow with and without, passive control. (a) Back pressure Integration of high bypass ratio engines on modern transonic wings for I without passive control. (b) Back pressure I with passive control. regional aircraft, E. Greff, K. Becker, M. Karwinand S. Rill, (c) Back pressure II without passive control. (d) Back pressure II pp 1-13 (Jan.) with passive control. (e) Back pressure III without passive control. (f) Back pressure III with passive control, pp 166-167 (May). NAVIER-STOKES Schlieren flowfield photograph, Z,./D = 2, p 211 (Jun./Jul.). The solution of the Navier-Stokes equations for two-dimensional com- Schlieren flowfield photograph, Z,./D = 3, p 211 (Jun./Jul.). pressible flows using a simple second order accurate algorithm, K.P. Schlieren flowfield photograph, Z,./D = 4, p 212 (Jun./Jui.). Sinhamahapatra, pp 131-137 (Apr.). Schlieren flowfield photograph, Z,./D = 5, p 212 (Jun./Jul.). Schlieren photograph, M = 1-53, Helium injection, / = 0-0088, p 217 NAVIGATION SYSTEMS (Jun./Jul.). Automatic navigation in the air and at sea, S.G. Smith, pp 183-194 Typical schlieren photographs, p 251 (Aug./Sept.). (Jun./Jul.). Blunt faced cylinder, Cp = 0-75, p 308 (Nov.). ORNITHOPTERS d,/d, = 0-75, g/d, = 0-25, Cp = 0-03, p 308 (Nov.). An aerodynamic model for flapping-wing flight, J.D. DeLaurier, pp Testbeds 125-130 (Apr.). Wing fan on the test bed, p 104 (Mar.). A study of mechanical flapping-wing flight, J.D. DeLaurier and J.M Windtunnel equipment Harris, pp 277-286 (Oct.). Windtunnel set-up, p 215 (Jun./Jul.). The development of an efficient ornithopter wing, J.D. DeLaurier, Photograph of cams, p 339 (Dec.) pp 153-162 (May). Windtunnel models PHOTOGRAPHS Windtunnel arrangement of three lift engine models in close line astern, Aircraft p 104 (Mar.). The E28/39 during taxying trials, p 65 (Feb.). Vectoring exhaust 15 in fan model in windtunnel, p 106 (Mar.). The E28/39 after first flight, p 66 (Feb.). Ornithopter wing in windtunnel, p 160 (May). Bell XP-59A Airacomet, p 66 (Feb.). PROPULSION Subject index Aeronautical Journal December1993 Machinery arrangements for Vtol transport aircraft, D.C. MacPhail, STRUCTURES AND STRUCTURAL DESIGN A.S. Jackson and E.S. Moore, pp 101-110, (Mar.). Orthotropic behaviour of shells and stability of uniaxially compressed cylinders, M.S. Hanna and A.W. Beshara, pp 111-117 (Mar.). The contributions of Power Jets Ltd to jet propulsion, G.B.R. Feilden, pp 62-72 (Feb.). Stress concentration factors in countersunk holes, J.B. Young and K.K. Lee, pp 267-276 (Oct.). Technical Note: Fuel consumption formulae and the general range equation, C.L. Bore, pp 118—120 (Mar.). SUPERSONIC FLOW An experimental study of the interaction of an unsteady shock with turbu- Technical Note: Non isentropic duct flow and the general drag wake lent boundary layer at Mach numbers of 1-3 and 1-5, J.A. Edwards traverse, C.L. Bore, pp 177-178 (May). and L.C. Squire, pp 337-348 (Dec.). Technical Note: Optimisation of constant altitude-constant airspeed flight Experimental study of overexpanded supersonic jet impingement on a for piston prop aircraft, S.J. Ojha, pp 145—148 (Apr.) double wedge deflector, J.K. Prasad, R.C. Metha and A.K. Seekanth, Technical Note: Propulsion streamtubes in supersonic flow and supercriti- pp 209-214 (Jun./Jul.). cal intake cowl, C.L. Bore, pp 257-259 (Aug./Sept.). TESTING Technical Note: Rotary jet thrust augmentors — the fallacy of Foa’s A pressure instrument to measure skin friction in turbulent boundary theory and the jet fan augmentor, C.L. Bore, pp 328-331 (Nov.). layers on smooth and non-smooth walls, P.V. Storm and B.G. Newman, pp 25-32 (Jan.). Technical Note: The Stream Force Theorem and applications to propul- sion, C.L. Bore, pp 138-144 (Apr.). Erratum: A pressure instrument to measure skin friction in turbulent boundary layers on smooth and non-smooth walls, P.V. Storm and ROAD VECHICLES B.G. Newman, p 208 (Jun./Jul.). The 33rd Lanchester Lecture. Automobile aerodynamics — the effects of airflow on road, racing and record breaking cars, J.L. Stollery, pp A summary of further measurements of steady and oscillatory pressures on 307-313 (Nov.). a rectangular wing, D.G. Mabey, B.L. Welsh and C.R. Pyne, pp 195-207 (Jun./Jul.). ROTORCRAFT A generic helicopter rotor model for helicopter flight simulation, M. Technical Note: The use of a Flame lIonisation Detector for mass fraction Chaimovich, A. Rosen and O. Rand, pp 14—24 (Jan.). measurement in short duration windtunnels, I.N.R. Bowman and J.A. Edwards, pp 215-217 (Jun./Jul.). ROYAL AERONAUTICAL SOCIETY LECTURES Automatic navigation in the air and at sea, S.G. Smith, pp 183-194 TRANSONIC FLOW (Jun./Jul.). Cavity drag at transonic speeds, L.C. Squire and S.H. Nasser, pp 247-256 The 11th Sir Sydney Camm Lecture. Supporting the Royal Air Force — (Aug./Sept.). the challenge for Logistics Command approaching the 21st century, Computational modelling of shock wave/boundary layer interaction with a R.J.M. Alcock, pp 223-229 (Aug./Sept.). cell-vertex scheme and transport models of turbulence, M.A. Leschziner, K.P. Dimitriadis and G. Page, pp 43-61 (Feb.). The 33rd Lanchester Lecture. Automobile aerodynamics — the effects of airflow on road, racing and record breaking cars, J.L. Stollery, pp Transonic shockwave/turbulent boundary layer interactions on a porous 307-313 (Nov.). surface, N. Chokani and L.C. Squire, pp 163-170 (May). The contributions of Power Jets Ltd to jet propulsion, G.B.R. Feilden, Self adaptive mesh refinement for the computation of steady, compress- pp 62-72 (Feb.). ible, viscous flows, J. Fischer, pp 357-368 (Dec.). Technical Note: Fuel consumption formulae and the general range TURBULENCE equation, C.L. Bore, pp 118-120 (Mar.). A pressure instrument to measure skin friction in turbulent boundary Technical Note: Non isentropic duct flow and the general drag wake layers on smooth and non-smooth walls, P.V. Storm and B.G. traverse, C.L. Bore, pp 177-178 (May). Newman, pp 25-32 (Jan.). Technical Note: Propulsion streamtubes in supersonic flow and supercriti- Erratum: A pressure instrument to measure skin friction in turbulent cal intake cowl, C.L. Bore, pp 257-259 (Aug./Sept.). boundary layers on smooth and non-smooth walls, P.V. Storm and B.G. Newman, p 208 (Jun./Jul.). Technical Note: Rotary jet thrust augmentors — the fallacy of Foa’s theory and the jet fan augmentor, C.L. Bore, pp 328-331 (Nov.). VORTICES Experiments on a 60° delta wing with vortex flaps and vortex plates, Technical Note: The Stream Force Theorem and applications to propul- K. Rinole, pp 33-38 (Jan.). sion, C.L. Bore, pp 138-144 (Apr.). WINDTUNNELS ROYAL AERONAUTICAL SOCIETY SYMPOSIA A pressure instrument to measure skin friction in turbulent boundary An economic puzzle for airline management — how to recover mandatory layers on smooth and non-smooth walls, P.V. Storm and B.G. investments, J.M. Mariani, pp 368-370 (Dec.). Newman, pp 25-32 (Jan.). SHOCK WAVE-BOUNDARY LAYER INTERACTION Erratum: A pressure instrument to measure skin friction in turbulent An experimental study of the interaction of an unsteady shock with turbu- boundary layers on smooth and non-smooth walls, P.V. Storm and lent boundary layer at Mach numbers of 1-3 and 1-5, J.A. Edwards B.G. Newman, p 208 (Jun./Jul.). and L.C. Squire, pp 337-348 (Dec.). Incompressible flow in contracting ducts, J.C. Gibbings, pp 230-246 Computational modelling of shock wave/boundary layer interaction with a (Aug./Sept.). cell-vertex scheme and transport models of turbulence, Technical Note: The use of a Flame Ionisation Detector for mass fraction M.A. Leschziner, K.P. Dimitriadis and G. Page, pp 43-61 (Feb.). measurement in short duration windtunnels, IN.R. Bowman and Transonic shockwave/turbulent boundary layer interactions on a porous J.A. Edwards, pp 215-217 (Jun./Jul.). surface, N. Chokani and L.C. Squire, pp 163—170 (May). WINGS SIMULATION An aerodynamic model for flapping-wing flight, J.D. DeLaurier, A generic helicopter rotor model for helicopter flight simulation, pp 125-130 (Apr.). M.Chaimovich, A. Rosen and O. Rand, pp 14—24 (Jan.). A study of mechanical flapping-wing flight, J.D. DeLaurier and J.M. Harris, pp 277—286 (Oct.). STABILITY AND CONTROL Stability augmentation of a sailplane in towed flight, G. de Matteis and The development of an efficient ornithopter wing, J.D. DeLaurier, W. Tamilia, pp 349-358 (Dec.). pp 153-162 (May). Aeronautical Journal December1993 Subject index AUTHOR INDEX AKSOY, H. and SO, R.M.C. GIBBINGS, J.C. Gas jets in an arbitrary stream, pp 287—295 (Oct.). Incompressible flow in contracting ducts, pp 230-246 (Aug./Sept.). ALCOCK, R.J.M. GREFF, E., BECKER, K., KARWIN, M. AND RILL, S. The 11th Sir Sydney Camm Lecture. Supporting the Royal Air Force — Integration of high bypass ratio engines on modern transonic wings for the challenge for Logistics Command approaching the 21st century, regional aircraft, pp 1-13 (Jan.). pp 223-229 (Aug./Sept.). GUGLIERI, G. and QUAGLIOTTIL, F. BECKER, K., GREFF, E., KARWIN, M. and RILL, S. Windtunnel experimental investigation of a high performance aircraft Integration of high bypass ratio engines on modern transonic wings for model, pp 73-80 (Feb.). regional aircraft, pp 1-13 (Jan.). HANNA, M.S. and BESHARA, A.W. BESHARA, A.W. and HANNA, MLS. Orthotropic behaviour of shells and stability of uniaxially compressed Orthotropic behaviour of shells and stability of uniaxially compressed cylinders, pp 111-117 (Mar.). cylinders, pp 111-117 (Mar.). HARRIS, J.M. and DELAURIER, J.D. BOWMAN, L.N.R. and EDWARDS, J.A. A study of mechanical flapping—wing ‘light, pp 277-286 (Oct.). Technical Note: The use of a Flame Ionisation Detector for mass fraction measurement in short duration windtunnels, pp 215-217 (Jun./Jul.). JACKSON, A.S., MACPHAIL, D.C. and MOORE, E.S. Machinery arrangements for Vtol transport aircraft, pp 101-110, (Mar.). BORE, C.L. Technical Note: Fuel consumption formulae and the general range equa- KARWIN, M., GREFF, E., BECKER, K. and RILL, S. tion, pp 118—120 (Mar.). Integration of high bypass ratio engines on modern transonic wings for regional aircraft, pp 1-13 (Jan.). Technical Note: The Stream Force Theorem and applications to propul- sion, pp 138— 144 (Apr.). LAHA, MLK. A vortex lattice method for thin wings oscillating in ideal flow, pp Technical Note: Non isentropic duct flow and the general drag wake 314-320 (Nov.). traverse, pp 177-178 (May). LEE, K.K. and YOUNG, J.B. Technical Note: Propulsion streamtubes in supersonic flow and supercriti- Stress concentration factors in countersunk holes, pp 267-276 (Oct.). cal intake cowl, pp 257-259 (Aug./Sept.). LESCHZINER, M.A., DIMITRIADIS, K.P. and PAGE, G. Technical Note: Rotary jet thrust augmentors — the fallacy of Foa’s theory Computational modelling of shock wave/boundary layer interaction with a and the jet fan augmentor, pp 328-331 (Nov.). cell—vertex scheme and transport models of turbulence, pp 43-61 (Feb.). CHAIMOVICH, M., ROSEN, A. and RAND, O. A generic helicopter rotor model for helicopter flight simulation, pp 14-24 MABEY, D.G., WELSH, B.L. and PYNE, C.R. (Jan.). A summary of further measurements of steady and oscillatory pressures on a rectangular wing, pp 195-207 (Jun./Jul.). CHOKANI, N. and SQUIRE, L.C. Transonic shockwave/turbulent boundary layer interactions on a porous MacPHAIL, D.C., JACKSON, A.S. and MOORE, E.S. surface, pp 163-170 (May). Machinery arrangements for Vtol transport aircraft, pp 101-110, (Mar.). DELAURIER, J.D. MARIANI, J.M. An aerodynamic model for flapping-wing flight, pp 125—130 (Apr.) An economic puzzle for airline management — how to recover mandatory investments, pp 368-370 (Dec.). The development of an efficient ornithopter wing, pp 153-162 (May). MEHTA, R.C., PRASAD, J.K. and SEEKANTH, A.K. DELAURIER, J.D. AND HARRIS, J.M. Experimental study of overexpanded supersonic jet impingement on a A study of mechanical flapping-wing flight, pp 277-286 (Oct.). double wedge deflector, pp 209-214 (Jun./Jul.). DE MATTEIS, G. and TAMILIA, W. MILLER, P. and WILSON, M. Stability augmentation of a sailplane in towed flight, pp 349-358 (Dec.). Wall jets created by single and twin high pressure jet impingement, pp 87-100, (Mar.). DIMITRIADIS, K.P., LESCHZINER, M.A. and PAGE, G. Computational modelling of shock wave/boundary layer interaction with a MOORE, E.S., MACPHAIL, D.C. and JACKSON, A.S. cell-vertex scheme and transport models of turbulence, pp 43-61 Machinery arrangements for Vtol transport aircraft, pp 101—110, (Mar.). (Feb.). MOUSTAFA, G.H. EDWARDS, J.A. and BOWMAN, L.N.R. Further study of high speed single free jets, pp 171-176 (May). Technical Note: The use of a Flame Ionisation Detector for mass fraction measurement in short duration windtunnels, pp 215-217 (Jun./Jul.). NASSER, S.H. and SQUIRE L.C. Cavity drag at transonic speeds, pp 247-256 (Aug./Sept.). EDWARDS, J.A. and SQUIRE, L.C. An experimental study of the interaction of an unsteady shock with turbu- NEWMAN, B.G. and STORM, P.V. lent boundary layer at Mach numbers of 1.3 and 1.5, pp 337-348 A pressure instrument to measure skin friction in turbulent boundary (Dec.). layers on smooth and non-smooth walls, pp 25—32 (Jan.). FEILDEN, G.B.R. Erratum: A pressure instrument to measure skin friction in turbulent The contributions of Power Jets Ltd to jet propulsion, pp 62—72 (Feb.). boundary layers on smooth and non-smooth walls, p 208 (Jun./Jul.). FISCHER, J. NEWMAN, S.J. Self adaptive mesh refinement for the computation of steady, compress- Engineering Note: The use of colour graphics to show streamlines in two ible, viscous flows, pp 357-368 (Dec.). dimensional flow, pp 296-297 (Oct.). Aeronautical Journal December1993