Unsteady motion of airfoils with boundary-layer separation

AIAA Journal

Volumn 14, Issue 2, 1976, Pages 216-220

  Sears, W R ^a  

^a UNIVERSITY OF ARIZONA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW OF FLUIDS - BOUNDARY LAYER;

AERODYNAMICS;

EID: 0016918815     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.7072     Document Type: Article

References (9)

1. Howarth, L., “The Theoretical Determination of the Lift Coefficient for a Thin Elliptic Cylinder,” Proceedings of the Royal Society of London, Vol. 149A, 1935, pp. 558-586.
2. Sears, W.R., “Some Recent Developments in Airfoil Theory,” Journal of Aeronautical Science, Vol. 23, No. 5, May 1956, pp. 490-499.
3. Moore, F.K., “Lift Hysteresis at Stall as an Unsteady Boundary-Layer Phenomenon,” TN 3571, 1955, NACA.
4. Von Karman, T. and Sears, W.R., “Airfoil Theory for NonUniform Motion,” Journal of Aeronautical Science, Vol. 5, No. 10, Aug. 1938, pp. 379-390.
5. Goldstein, S., “A Theory of Aerofoils of Small Thickness, Parts I and II,” 5804 (Ae 1976) and 6156 (Ae 1976a), 1942, Aeronautical Research Council, London.
6. Lighthill, M.J., “A New Approach to Thin Aerofoil Theory,” Aeronautical Quarterly, Vol. 3, Nov. 1951, pp. 193-210.
7. Sears, W.R., “A Systematic Presentation of the Theory of Thin Airfoils in Non-Uniform Flow,” Thesis, 1938, California Institute of Technology, Pasadena, Calif.
8. Sears, W.R., “A Contribution to the Airfoil Theory for NonUniform Motion,” Proceedings of the 5th International Congress of Applied Mechanics, 1938.
9. Sears, W.R. and Kuethe, A.M., “The Growth of the Circulation of an Airfoil Flying through a Gust,” Journal of Aeronautical Science, Vol. 6, No. 9, July 1939, pp. 376-378