Volume 97 - February 1993
Research Article
Wall jets created by single and twin high pressure jet impingement
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- 04 July 2016, pp. 87-100
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Stress concentration factors in countersunk holes
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- 04 July 2016, pp. 267-276
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Computational modelling of shock wave/boundary layer interaction with a cell-vertex scheme and transport models of turbulence
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- 04 July 2016, pp. 43-61
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Integration of high bypass ratio engines on modern transonic wings for regional aircraft
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- 04 July 2016, pp. 1-13
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Automatic navigation in the air and at sea
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- 04 July 2016, pp. 183-194
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The development of an efficient ornithopter wing
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- 04 July 2016, pp. 153-162
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An aerodynamic model for flapping-wing flight
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- 04 July 2016, pp. 125-130
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The 33rd Lanchester Lecture. Automobile aerodynamics — the effects of airflow on road, racing and record breaking cars
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- 04 July 2016, pp. 307-313
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An experimental study of the interaction of an unsteady shock with a turbulent boundary layer at Mach numbers of 1.3 and 1.5
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- 04 July 2016, pp. 337-348
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The 11th Sir Sydney Camm Lecture. Supporting the Royal Air Force — the challenge for Logistics Command as we approach the 21st century
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- 04 July 2016, pp. 223-229
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The contributions of Power Jets Ltd to jet propulsion
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- 04 July 2016, pp. 62-72
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Incompressible flow in contracting ducts
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- 04 July 2016, pp. 230-246
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A study of mechanical flapping-wing flight
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- 04 July 2016, pp. 277-286
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A summary of further measurements of steady and oscillatory pressures on a rectangular wing
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- 04 July 2016, pp. 195-207
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The solution of the Navier-Stokes equations for two-dimensional compressible flows using a simple second order accurate algorithm
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- 04 July 2016, pp. 131-137
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A generic harmonic rotor model for helicopter flight simulation
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- 04 July 2016, pp. 14-24
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Transonic shockwave/turbulent boundary layer interactions on a porous surface
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- 04 July 2016, pp. 163-170
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Stability augmentation of a sailplane in towed flight
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- 04 July 2016, pp. 349-356
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Machinery arrangements for small Vtol transport aircraft
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- 04 July 2016, pp. 101-110
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A vortex lattice method for thin wings oscillating in ideal flow
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- 04 July 2016, pp. 314-320
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