The pitching delta wing

AIAA Journal

Volumn 23, Issue 11, 1985, Pages 1660-1665

  Gad El Hak, Mohamed ^a   Ho, Chih Ming ^a,b  

^a Flow Research Company   (United States)

^b UNIVERSITY OF SOUTHERN CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS - WINGS AND AIRFOILS; FLOW OF FLUIDS - VISUALIZATION;

LIFT PERFORMANCE; SEPARATED FLOW;

AIRCRAFT;

EID: 0022161641     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.9147     Document Type: Article

References (18)

1. Jones, R.T. and Cohen, D., High Speed Wing Theory, Princeton University Press, Princeton, NJ, 1960.
2. EUe, B.J., “An Investigation at Low Speed of the Flow Near the Apex of Thin Delta Wings with Sharp Leading Edges,” Aeronautical Research Council, R&M 3176, Jan. 1958.
3. Fink, P.T. and Taylor, J., “Some Early Experiments on Vortex Separation, Part II: Some Low Speed Experiments with 20 Degree Delta Wings,” Aeronautical Research Council, R&M 3489, Sept. 1966.
4. McAlister, K.W. and Carr, L.W., “Water Tunnel Visualization of Dynamic Stall,” Journal of Fluids Engineering, Vol. 101, Sept. 1979, pp. 376-380.
5. McCroskey, W.J., “Unsteady Airfoils,” Annual Review of Fluid Mechanics, Vol. 14, Jan. 1982, pp. 285-311.
6. Lambourne, N.C., Bryer, D.W., and Maybrey, J.F.M., “The Behaviour of the Leading-Edge Vortices Over a Delta Wing Following a Sudden Change of Incidence,” Aeronautical Research Council, R&M 3645, March 1969.
7. Gad-el-Hak, M., Blackwelder, R.F., and Riley, J.J., “On the Growth of Turbulent Regions in Laminar Boundary Layers,” Journal of Fluid Mechanics, Vol. 110, Sept. 1981, pp. 73-95.
8. Gad-el-Hak, M., Ho, C.-M., and Blackwelder, R.F., “A Visual Study of a Delta Wing in Steady and Unsteady Motion,” Unsteady Separated Flows, edited by M.S. Francis and M'.W. Luttges, University of Colorado, Colorado Springs, Aug. 1983, pp. 45-51.
9. Gad-el-Hak, M. and Blackwelder, R.F., “The Discrete Vortices from a Delta Wing,” AIAA Journal, Vol. 23, June 1985, pp. 961-962.
10. Williams, J.C., III, “Incompressible Boundary-Layer Separation,” Annual Review of Fluid Mechanics, Vol. 9, Jan. 1977, pp. 113-144.
11. Telionis, P.P., Unsteady Viscous Flows, Springer-Verlag, New York, 1981.
12. Didden, N. and Ho, C.-M., “Unsteady Separation in the Boundary Layer Produced by an Impinging Jet,” Journal of Fluid Mechanics, in press, 1985.
13. Ho, C.-M. and Nosseir, N.S.M., “Dynamics of an Impinging Jet. Part 1: The Feedback Mechanism,” Journal of Fluid Mechanics, Vol. 105, April 1981, pp. 119-142.
14. McAlister, K.W., Carr, L.W., and McCroskey, W.J., “Dynamic Stall Experiments on the NACA 0012 Airfoil,” NASA TP 1100, Jan. 1978.
15. Francis, M.S. and Keesee, J.E., “Airfoil Dynamic Stall Performance with Large Amplitude Motions,” submitted to AIAA Journal, 1985.
16. Fink, P.T., “Some Early Experiments on Vortex Separation, Part III: Further Experiments with 20 Degree Delta Wings,” Aeronautical Research Council, R&M 3489, Sept. 1966.
17. Freymuth, P., Bank, W., and Palmer, M., “Visualization of Accelerating Flow Around an Airfoil at High Angles of Attack,” Zeitschrift der Flugwissenschaft fuer Weltraumforschungs, Vol. 7, July 1983, pp. 392-400.
18. Gad-el-Hak, M. and Ho, C.-M., “Three Dimensional Effects on a Pitching Lifting Surface,” AIAA Paper 85-0041, Jan. 1985.