The effect of compressibility on suppression of dynamic stall using a slotted airfoil

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Carr, L W ^a   Chandrasekhara, M S ^b   Wilder, M C ^c   Noonan, K W ^d  

^a NASA AMES RESEARCH CENTER   (United States)

^b NAVAL POSTGRADUATE SCHOOL   (United States)

^c MCAT Inc   (United States)

^d NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; OSCILLATING FLOW;

AIRFOIL MOTIONS; DYNAMIC STALLS; FLOW DEVELOPMENT; INSTANTANEOUS PRESSURES; MULTI ELEMENT AIRFOILS; OSCILLATION CYCLES; POINT DIFFRACTION; STALL BOUNDARIES;

AIRFOILS;

EID: 84983113677     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. Carr, L. W., "Progress in Analysis and Prediction of Dynamic Stall," AIAA J of Aircraft, Vol. 25, No. 1, pg. 6-17, January 1988.
2. Carr, L. W., and McCroskey, W. J., "A Review of Recent Advances in Computational and Experimental Analysis of Dynamic Stall," Proceedings of the 1UTAM Symposium on Fluid Dynamics of High Angle of attack, Tokyo, Japan, September 13-17. 1992.
3. Carr, L. W., and Chandrasekhara, M. S., "Compressibility Effects on Dynamic Stall," Progress in Aerospace Sciences, Vol. 32, pp. 523-573, 1996.
4. Carr, L. W., and McAlister, K. W., "The Effect of a leading-Edge Slat on the Dynamic Stall of an Oscillating Airfoil," AIAA Paper 83-2533, AIAA/AHS Aircraft Design, Systems and Operations Meeting, Ft. Worth, TX, October 17-19, 1983.
5. Noonan, K. W., Allison, D. O., and Stanaway, S., "Investigation of a Slotted Rotorcraft Airfoil at Mach Numbers from 0. 20 to 0. 88 at Full-Scale Reynolds Numbers," AHS Aeromechanics Specialists Conference, San Francisco, CA, January 1994.
6. Noonan, K. W., private communication.
7. Noonan, K. W., "Aerodynamic Characteristics of a Rotorcraft Airfoil Designed for the Tip Region of a Main Rotor Blade," NASA TM 4264, 1991.
8. Carr, L. W., and Chandrasekhara, M. S., "Design and development of a Compressible Dynamic Stall facility," AIAA J of Aircraft, Vol. 29, No. 3, May-June 1992, pp. 314-318.
9. Brock, N. J., Chandrasekhara, M. S., and Carr, L. W., "A Real Time Interferometry System for Unsteady Flow Measurements," 1CIASF '91 Record, IEEE Publication 91CH3028-8, pp. 423-430.
10. Carr, L. W., Chandrasekhara, M. S., and Brock, N. J., "Quantitative Study of Unsteady Compressible Flow on an Oscillating Airfoil," AIAA J of Aircraft, V31, N4, pp. 892-898, 1994.
11. th Applied Aerodynamics Conference, Atlanta, GA, June 23-25, 1997.
12. DeHughes, P. P., McAlister, K. W., and Tung, C., "Effect of an Extendable Slat on the Stall Behavior of a VR-12 Airfoil," NASA TP-3407, 1993.
13. Reynolds, W. C, and Carr, L. W., "Review of Unsteady, Driven, Separated Flows," AIAA Paper 85-0527, AIAA Shear Flow Conference, Boulder, CO, March 12-14, 1985.