Design and development of a compressible dynamic stall facility

Journal of Aircraft

Volumn 29, Issue 3, 1992, Pages 314-318

  Carr, L W ^a   Chandrasekhara, M S ^b  

^a NASA AMES RESEARCH CENTER   (United States)

^b NAVAL POSTGRADUATE SCHOOL   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT - WINGS;

COMPRESSIBILITY EFFECTS; DYNAMIC STALL; STALL;

AERODYNAMICS;

EID: 0026869880     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.46163     Document Type: Article

References (11)

1. Carr, L. W., McAlister, K. W., and McCroskey, W. J., "Analysis of the Development of Dynamic Stall Based on Oscillating Airfoil Experiments," NASA TN-8382, Jan. 1977.
2. McCroskey, W. J., McAlister, K. W., Carr, L. W., Pucci, S. L., Lambert, O., and Indergand, R. F., "Dynamic Stall on Advanced Airfoil Sections," Journal of American Helicopter Society, July 1981, pp. 40-50.
3. Carr, L. W., "Progress in Analysis and Prediction of Dynamic Stall," Journal of Aircraft, Vol. 25, No. 1, 1988, pp. 6-17.
4. McAlister, K. W., and Carr, L. W., "Water-Tunnel Visualization of Dynamic Stall," Journal of Fluids Engineering, Vol. 101, No. 3, 1979, pp. 376-380.
5. Helin, H. E., Robinson, M. C., and Luttges, M. W., "Visualization of Dynamic Stall Controlled by Large Amplitude Pitching Motions," AIAA Paper 86-2281-CP, Aug. 1986.
6. Lee, G., Buell, D. A., and Licursi, J. P., "Laser Holographic Interferometry for an Unsteady Airfoil Undergoing Dynamic Stall," AIAA Journal, Vol. 22, No. 4, 1984, pp. 504-511.
7. McCroskey, W. J., and Fisher, R. K., "Detailed Aerodynamic Measurements on a Model Rotor in the Blade Stall Regime," Journal of the American Helicopter Society, Vol. 17, No. 1, Jan. 1972, pp. 20-30.
8. Davis, S. S., "Measurement of Discrete Vortex Noise in a Closed- Throat Wind Tunnel," AIAA Paper 75-488, March 1975.
9. Kadlec, R. A., and Davis, S. S., "Visualization of Quasiperiodic Flows," AIAA Paper 78-502R; see also AIAA Journal, Vol. 17, No. 11, 1979, pp. 1164-1169.
10. Sticht, C. D., "Development of Drive Mechanism for an Oscillating Airfoil," Symposium on Aerospace Mechanisms, NASA Langley Research Center, Hampton, VA, May 4-6, 1988.
11. Chandrasekhara, M. S., and Carr, L. W., "Flow Visualization Studies of the Effect of Mach Number on Dynamic Stall," Journal of Aircraft, Vol. 27, No. 3, 1990, pp. 516-522.