Abstract

^achmann, G. V. (ed.), Boundary Layer and Flow Control (Pergamon Press, New York, 1961), Vol. 1. 2 Schwarz, F. and Wuest, W., tests and wind-tunnel measurements on aerofoils with boundary layer suction for increasing maximum lift/' Paper 64-564, Fourth Congress of the International Council of the Aerospace Sciences, Paris (1964). 3 Schwarz, F., Flugversuche am Baumeister RW3a mit grenzschichtabsaugung zur Steigerung des Hochstauftriebs, Z.f.Flugwiss. 11 (1963). 4 Raspet, A., Cornish, J. J., and Bryant, G. D., Delay of the stall by suction through distributed perforations, IAS Preprint 587 (1956). 5 Cornish, J. J., Fixed wing STOL aircraft with distributed suction for extended latitude, American Society of Engineers Paper 60-AV-12 (1960). 6 Hurley, D. G. and Ruglen, N., The use of boundary layer control to establish free stream-line flows being an introduction to the free stream-line flap, Aerospace Research Lab. Rept. A109 (1958). 7 Head, M. R., Entrainmeiit in the turbulent boundary layer, Aeronautical Research Council R & M 3152 (1958). Black, T. J. and Sarnecki, A. J., The turbulent boundary layer with suction or injection, Aeronautical Research Council R & M 3387 (1964). 9 Thompson, B. G. J., A critical review of existing methods of calculating the turbulent boundary layer, Aeronautical Research Council 26, 109 (1964). 10 Thompson, B. G. J., The calculation of shape-factor development in incompressible turbulent boundary layers with or without transpiration, AGARDograph 97, pp. 159-191 (1965). 11 Edwards, B. J., The take-off and landing performance of high-lift aircraft, M.Sc. Thesis, Cambridge Univ. (1960). 12 Mair, W. A. and Edwards, B. J., A parametric study of takeoff and landing distances for high-lift aircraft, Aeronautical Research Council C.P. 823 (1965). 13 Johnston, G. W., Factors affecting the field length of STOL aircraft, AGARD Rept. 81 (1956). 14 Sutcliff, P. L., Merrick, V. K., and Howell, A. R,, Aerodynamic and propulsion considerations of minimum-field aircraft, 8th Anglo-American Aeronautical Conference (1961). 15 Wimpress, J. K., Shortening the take-off and landing distances of high speed aircraft, AGARD Flight Mechanics Panel 26th Meeting, Paris (June 1965). 16 Young, A. D., A note on ground effect on the lift due to a jet flap, Aeronautical Research Council 19, p. 971 (1958). 17 Head, M. R. and Clark, D. G., 'Flight experiments on suction for high lift, AIAA Paper 65-750 (November 1965).

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