Thin-Airfoil Theory of an Ejector-Flapped Wing Section
1975; American Institute of Aeronautics and Astronautics; Volume: 12; Issue: 1 Linguagem: Inglês
10.2514/3.59797
ISSN1533-3868
Autores Tópico(s)Particle Dynamics in Fluid Flows
ResumoSpence, D. A., Lift on a Thin Aerofoil with a Blown Flap, RAE TN Aero 2450, May 1956, Royal Aircraft Establishment, Farnborough, England. Herold, A. C., A Two-Dimensional, Interative Solution for the Jet Flap, CR-2190, Feb. 1973, NASA. Dvorak, F. A., Calculation of Turbulent Boundary Layers and Wall Jets over Curved Surfaces, AIAA Journal, Vol. 11, No. 4, April 1973, pp. 517-524. Goradia, S. H. and Colwell, G. T., Parametric Study of a Two-Dimensional Turbulent Wall Jet in a Moving Stream with Arbitrary Pressure Gradient, AIAA Journal, Vol. 9, No. 11, Nov. 1971, pp. 2156-2165. Kacker, S. C. and Whitelaw, J. H., Some Properties of the Two-Dimensional Turbulent Wall Jet in a Moving Stream, Journal of Applied Mechanics, Vol. 35, No. 4, Dec. 1968, pp. 641651. Schlichting, H., Boundary Layer Theory, McGraw-Hill, New York, 1968, pp. 590-609. ^Bangert, L. H., Turbulent Wall Jet with an Initial Boundary Layer, AIAA Paper 71-612, Palo Alto, Calif., 1971. Gartshore, I. S. and Newman, B. C., Turbulent Wall Jet in an Arbitrary Pressure Gradient, The Aeronautical Quarterly, Vol. XX, Pt. I, Feb. 1969, pp. 25-56. Coles, D., Proceedings, Computation of Turbulent Boundary Layers—1968, AFOSP-IFP-Stanford Conference, Vol. II, Aug. 1825, 1968, pp. 1-46. Lawford, J. A. and Foster, D. N., Low Speed Wind Tunnel Tests on a Wing Section with Plain Leadingand Trailing-Edge Flaps Having Boundary Layer Control by Blowing, RAE TR 69078, April 1969, Royal Aircraft Establishment, Farnborough, England.
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