Heat flux gage studies of compressible dynamic stall

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Chandrasekhara, M S ^a   Wilder, M C ^b  

^a NAVAL POSTGRADUATE SCHOOL   (United States)

^b NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 33746604604     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. M.S. Chandrasekhara, M.C. Wilder, L.W. Carr, Competing Mechanisms of Compressible Dynamic Stall, AIAA Journal, Vol. 36, No. 3, 1998, pp. 387-393.
2. J.W. Kiedaisch, M. Acharya, Investigation of Incipient Dynamic Stall Over Pitching Airfoils Using Hot-Film Sensors, AIAA 97-0656, 35th Aerospace Sciences Meeting and Exhibit, Jan. 6-10, 1997, Reno, NV.
3. T. Lee, S. Basu, Measurement of Unsteady Boundary Layer Developed on an Oscillating Airfoil Using Multiple Hot-Film Sensors, Experiments in Fluids, Vol. 25, No. 1,1998, pp. 108-117.
4. S.J. Schreck, W.E. Faller, H.E. Helin Pitch Rate and Reynolds Number Effects on Unsteady Boundary Layer Transition and Separation, AIAA Journal of Aircraft, Vol. 35, No. 1, 1998, pp. 46-52.
5. S.J. Schreck, W.E. Faller, M.C. Robinson, Unsteady Separation Processes and Leading Edge Vortex Precursors: Pitch Rate and Reynolds Number Influences, AIAA 2000-2605, Fluids 2000 Conference, Jun. 19-22, 2000, Denver, CO.
6. A. Nakayama, J.P. Stack, J.C. Lin, W.O. Valarezo, Surface Hot-Film Technique for Measurements of Transition, Separation, and Reattachment Points, AIAA 93-2918, 24th Fluid Dynamics Conference, Jul. 6-9, 1993, Orlando, FL.
7. J.P. Stack, S.M. Mangalam, S.A. Berry, A Unique Measurement Technique to Study Laminar-Separation Bubble Characteristics on an Airfoil, AIAA 87-1271, 19th Fluid Dynamics, Plasma Dynamics and Lasers Conference, Jun. 8-10, 1987, Honolulu, HI.
8. Cui and D.D. Knight, Parallel Computation of the 2-D Navier-Stokes Flowfield of a Pitching Airfoil, Computational Fluid Dynamics, 1995, Vol. 4, pp. 111-135.
9. W. Geissler, L.W. Carr, M.S. Chandrasekhara, M.C. Wilder and H. Sobieczky, Compressible Dynamic Stall Calculations Incorporating Transition Modeling for Variable Geometry Airfoils, AIAA Paper 98-0705, Reno, NV, Jan. 1998.
10. S. Ahmed, and M.S. Chandrasekhara, Reattachment Studies of an Oscillating Airfoil Dynamic Stall Flow Field, (AIAA Paper 91-3225), AIAA Journal, Vol. 32, No. 5, May 1994, pp. 1006-1012.