Transition effects on compressible dynamic stall of transiently pitching airfoils

AIAA 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference, 1993

Volumn , Issue , 1993, Pages

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

^a Navy NASA Joint Institute of Aeronautics and MCAT Inc   (United States)

^b NAVAL POSTGRADUATE SCHOOL   (United States)

^c NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRFOILS; ANGLE OF ATTACK; ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYERS; FLUID DYNAMICS; LAMINAR FLOW; MAGNETOHYDRODYNAMICS; TURBULENCE; VORTEX FLOW;

ANGLES OF ATTACK; DYNAMIC STALLS; LAMINAR SEPARATION BUBBLE; LOW MACH NUMBERS; OSCILLATING AIRFOIL; PITCHING AIRFOILS; SHOCK/BOUNDARY LAYER INTERACTIONS; VORTEX FORMATION;

MACH NUMBER;

EID: 85006511977     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Chandrasekhara, M.S. and Carr, L.W., “Flow Visualization Studies of the Mach Number Effects on the Dynamic Stall of an Oscillating Airfoil”, Journal of Aircraft, Vol. 27, No. 6, pp. 516-522.
2. Chandrasckhara, M.S., Ahmed, S. and Carr, L.W., “Schlieren Studies of Compressibility Effects on Dynamic Stall of Airfoils in Transient Pitching Motion”, Journal of Aircraft, Vol. 30, No. 2, pp. 213-220.
3. Chandrasekhara, M.S. and Carr, L.W., and Wilder, M.C., “Interferometric Investigations of Compressible Dynamic Stall Over a Transiently Pitching Airfoil”, AIAA Paper 93-0211, Accepted for publication in AIAA Journal
4. McCroskey, W.J., McAlister, K.W., Carr, L.W., Pucci, S.L., Lambert, O., and Indergrand, R.F., “Dynamic Stall on Advanced Airfoil Sections”, Journal of American Helicopters Society, Vol. 26, No. 3, pp. 40-50.
5. Lorber, P.F. and Carta, F.O., “Unsteady Stall Penetration Experiments at High Reynolds Number”, AFOSR-TR-87-1202, April 1987.
6. Carr, L.W., Chandrasekhara, M.S., Ahmed, S., and Brock, N.J., “A Study of Dynamic Stall Using Real Time Interferometry” , AIAA Paper 91-0007, Accepted for publication in Journal of Aircraft.
7. Gostelow, J.P., Blunden, A.R., and Walker, G.J., “Effects of Free-Stream Turbulence and Adverse Pressure Gradients on Boundary Layer Transition”, ASME Paper No. 92-G7-380, presented at the International gas Turbine and Aero Engine Congress and Exposition, Cologne, Germany, June 1-4, 1092.
8. Visbal, M.R., “Effect of Compressibility on Dynamic Stall of a Pitching Airfoil”, AIAA Paper No. 88-0132, Jan. 1988.
9. Chandrasekhara, M.S., Carr, L.W., Ekaterinaris, J.A., and Platzer, M.F., “Interferometry and Computational Studies of an Oscillating Airfoil Compressible Dynamic Stall”, Proceedings of The bth Asian Congress of Fluid Mechanics, Vol. 2, pp. 1047-1050, Ed. K.S. Chang and D.H. Choi, Aug. 1992.
10. Carr, L.W., and Chandrasekhara, M.S., “Design and Development of a Compressible Dynamic Stall Facility”, Journal of Aircraft, Vol. 29, No. 3, pp. 314-318.
11. Chandrasekhara M.S. and Carr, L.W., “Design and Development of a Facility for Compressible Dynamic Stall Studies of a Rapidly Pitching Airfoil”, ICIASF'89 RECORD, IEEE Publication 89-C1127623, pp. 29-37.
12. Brock, N.J., Chandrasekhara, M.S., and Carr, L.W., “A Real Time Interferometry System for Unsteady Flow Measurements”, ICIASF'91 RECORD, IEEE Publication 91-CII3028-8, pp. 423-430.
13. Pope, A., and Goin, K.L., High Speed Wind Tunnel Testing, Kraeger Publishing Company, New York, NY, 1978.
14. McAlister, K.W, Pucci, S.L., McCroskey, W.J., and Carr, L.W,, “An Experimental Study of Dynamic Stall of Advanced Airfoil Sections, Volume 2, Pressure and Force Data”, NASA TM 84245, Sept. 1992.
15. Cho, Y.C., Carr, L.W., and Chandrasekhara, M.S., “Correction to Fringe Distortion due to Flow Density Gradients in Optical Interferometry” AIAA Paper No. 93-0631, presented at the 31st Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan, 11-14, 1993.