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Assessment of lift augmentation devices

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  • D.M., MCRAE -HAWKER SIDDELEY A VIA TION L TD, UK: The aerodynamics of mechanical high-lift devices
  • H.P., HORTON -VKI: Fundamental aspects of separation under high-lift conditions
  • B., VAN DEN BERG -NLR, NETHERLANDS: Some notes on 2D high-lift tests in wind tunnels
  • J., VON DER DECKEN -TH BRAUNSCHWEIG, FR GERMANY: Aerodynamics of pneumatic high-lift devices
  • C., RUSSELL -BRITISH AIRCRAFT CORP. , UK: Model testing requirements and techniques for high-lift schemes-3D aspects
  • L.B., GRATZER -THE BOEING CO, USA: Analysis of transport applications for high-lift schemes
  • R., TAISSIERE -BREGUET AVIATION, FRANCE: Analysis of combat aircraft
    Applications of the lift
    Augmentation devices
  • K.P., EYRE -AIRCRAFT & ARMAMENT EXPERIMENTAL EST., UK: Flight testing military transport aircraft for clearance in the STOL role
  • J.A., HOOPER & E.A., WHITE -ROLLS-ROYCE L TD, UK: Lift augmentation devices and their effect on the engine
  • E.A., WHITE & H.C., HILLIER -ROLLS-ROYCE LTD/BRISTOL ENGINE DIV., UK: Thermodynamic problems and some possible solutions
  • H.T., BOWLING -LOCKHEED-GEORGIACO, USA: Optimizing the propulsion/lift system for turbofan STOL aircraft considering cost-effectiveness

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