Volume 101 - March 1997
Research Article
V-22 Osprey aerodynamic development — a progress review
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- 04 July 2016, pp. 231-244
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A parametric windtunnel test on rotorcraft aerodynamics and aeroacoustics (Helishape) — test procedures and representative results
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- 04 July 2016, pp. 143-154
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An analytical model for ACSR approach to vibration reduction in a helicopter rotor-flexible fuselage system
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- 04 July 2016, pp. 399-408
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The use of inverse simulation for preliminary assessment of helicopter handling qualities
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- 04 July 2016, pp. 287-294
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Homogeneous wall boundary condition for oscillatory flow in slotted tunnels
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- 04 July 2016, pp. 99-110
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Future large aircraft design — the delta with suction
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- 04 July 2016, pp. 187-198
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An airborne windshear detection system
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- 04 July 2016, pp. 447-456
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Multidisciplinary optimisation of a supersonic transport using design of experiments theory and response surface modelling
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- 04 July 2016, pp. 347-356
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A cartesian cut cell method for compressible flows Part A: static body problems
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- 04 July 2016, pp. 47-56
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Validation of a blade-element helicopter model for large-amplitude manoeuvres
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- 04 July 2016, pp. 1-8
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Experimental investigation of vortex dynamics on a 65° delta wing in sideslip
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- 04 July 2016, pp. 111-120
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Neural network models of human operator performance
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- 04 July 2016, pp. 155-158
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Windtunnel testing of parachutes for the Huygens probe
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- 04 July 2016, pp. 357-364
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International obligations as regards safety in international civil aviation
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- 04 July 2016, pp. 457-466
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A cartesian cut cell method for compressible flows Part B: moving body problems
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- 04 July 2016, pp. 57-65
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The reduction of numerical entropy generated by unsteady Shockwaves
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- 04 July 2016, pp. 9-16
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A cell-vertex upwind scheme for two-dimensional supersonic Euler flows
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- 04 July 2016, pp. 199-208
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Studies of vortex flaps for different sweepback angle delta wings
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- 04 July 2016, pp. 409-416
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Low thrust orbit raising with J2 regression
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- 04 July 2016, pp. 295-298
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V-22 flight test update
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- 04 July 2016, pp. 245-254
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