[1] Holzhauser, C.A., Innis, R. C., and Vomaske, R. F., A flight and simulator study of the handling qualities of a deflected slipstream STOL seaplane having four propellers and boundary layer control[J].NASA TN D-2964, 1965.
[2] Anderson, S.B.An examination of handling qualities criteria for V/STOL aircraft[J].NASA TN D-331, 1960.
[3] Kuhn, R.E., Semi-empirical procedure for estimating lift and drag characteristics of propeller-wing-fiap configurations for vertical-and-short-take-off-and landing airplanes[J].NASA Memo. 1-16-59L, 1959.
[4] Petrov A.V. Aerodynamics of aircraft with wing-powered lift systems[J].AIAA-93-4836, 1993.
[5] Baysal O., “Aerodynamic Shape Optimization: Me-thods and Applications”, World Aviation onference, San Francisco, CA, 1999.
[6]Sobieczky H.Parametric airfoils and wings[J].Note on Numerical Fluid Mechanics, 1998, 68(1):71-88
[7] Jameson A.Aerodynamic shape optimization for aircraft design[R],Beijing:6th World Congress of Compu-tational Machanics,2004.
[8] Earl C.Watson, Jules B.Dods, The effects of blowing over various trailing-edge flaps on an NACA 0006 airfoil cestion, comparisons with various types of flaps on other airfoil sections, and an analysis of flow and power relationships for blowing systems[J]. NASA TN D-8293, 1976.
[9] Curt A.Holzbauser, Robert C.Innis, A flight and simulator study of the handing qualities of a deflected slipstream STOL seaplane having four propellers and boundary-laryer control[J]., NASA TN D-2966, 1965.
[10] J.A. Lawford,Low-Speed Wind-Tunnel Tests on an Unswept Wing-Fuselage Model of Aspect Ratio 9.8,with Tangential Blowing over Trailing-Edge Flaps and Ailerons,including the Effect of Slipstream[J].NASA TN D-1108, 1970.
[11] Rolls, L.S. and Innis, R. C.A flight evaluation of a wingshroud-blowing boundary layer control system applied to the flaps of an F9F-4 airplane[J], NACA RMA 55K01, 1956.
[12] Falarski, M.D.and Koenig, D.G, Aerodynamic characte-ristics of a large-scale model with a sweep wing and augmented jet flap[J]., NASA TM X-62029, July 1971.
[13] G.S.Jones, S.A.Viken, An Active Flow Circulation Controlled Flap Concept for General Aviation Aircraft Applications[J], AIAA-2003-3157.
[14] Garl L.Gentry, Jr., M. A.Aerodynamic Characteristics of a Propeller-Powered High-Lift Semispan Wing[J].NASA TM 4541, 1994.
[15] Koenig, P.G. and Kiyoshi, A. Large scale wind tunnel tests of an airplane model with a 45° swept-back wing of aspect ratio 2.8 with area suction applied to trailing edge flaps and with several wing leading edge mod-ifications[J].NACA RM A56H08, 1956.
|