Compressible dynamic stall calculations incorporating transition modeling for variable geometry airfoils

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Geissler, W ^a   Carr, L W ^b   Chandrasekhara, M S ^c   Wilder, M C ^d   Sobieczky, H ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b NASA AMES RESEARCH CENTER   (United States)

^c NAVAL POSTGRADUATE SCHOOL   (United States)

^d MCAT Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; AIRFOILS; REYNOLDS NUMBER;

DYNAMIC STALLS; FLOW CONDITION; FREESTREAM MACH NUMBER; INTERFEROGRAMS; LARGE-AMPLITUDE PITCHING; PHYSICAL ASPECTS; TRANSITION MODEL; VARIABLE GEOMETRY;

DYNAMICS;

EID: 84983208333     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. Carr, L.W., Chandrasekhara, M.S., and Brock, N., "A Quantitative Study of Unsteady Compressible Flow on an Oscillating Airfoil," Journal of Aircraft, Vol. 31, No. 4, Jul.-Aug. 1994, pp. 592-598.
2. Srinivasan, G.R., Ekaterinaris, J.A., and McCroskey, W.J., "Evaluation of Turbulence Models for Unsteady Flows of an Oscillating Airfoil," Computers & Fluids, Vol. 24, No. 7, 1995, pp. 833-861.
3. Geissler, W., "Instationäres Navier-Stokes-Verfahren für beschleunigt bewegte Profile mit Ablösung," DLR German Aerospace Research Establishment, DLR-FB-92-03, Göttingen, Germany, Jan. 1992, pp. 1-68.
4. Choudhuri, P.G., Knight, D.D., and Visbal, M.R., "Two-Dimensional Unsteady Leading Edge Separation on a Pitching Airfoil," AIAA Journal, Vol. 32, No. 4, April 1994, pp. 673-681.
5. Ekaterinaris, J.A., and Menter, F.R., "Computation of Oscillating Airfoil Flows with One-and Two-Equation Turbulence Models," AIAA Journal, Vol. 32, No. 12, 1994, pp. 2359-2365.
6. Chandrasekhara, M.S., Wilder, M.C., and Carr, L.W., "Control of Flow Separation Using Adaptive Airfoils," AIAA Paper No. 97-0655.
7. Geissler, W., and Sobieczky, H., "Dynamic Stall Control by Variable Airfoil Camber," AGARD-CP-552, Oct. 1994, pp. 6.1-6.10.
8. Geissler, W., and Raffel, M., "Dynamic Stall Control by Airfoil Deformation," European Rotorcraft Forum, Cuomo, Italy, 1993.
9. Ekaterinaris J.A., and Platzer, M.F., "Numerical Investigation of Stall Flutter," ASME Journal of Turbomachinery, Vol. 118, Apr. 1996, pp. 197-203.
10. Ekaterinaris, J.A., Chandrasekhara, M.S., and Platzer, M.F., "Analysis of Low Reynolds Number Airfoil Rows," Journal of Aircraft, Vol. 32, No. 3, May-Jun. 1995, pp.625-630.
11. Van Dyken, R.D., Ekaterinaris, J.A., Chandrasekhara, M.S., and Platzer, M.F., "Analysis of Compressible Light Dynamic Stall Flow at Transitional Reynolds Numbers," AIAA Journal, Vol. 34, No. 7, Jul. 1996, pp. 1420-1427.
12. Cho, Y.C., Carr, L.W., and Chandrasekhara, M.S., "Corrections to Fringe Distortion due to Flow Density Gradients in Optical Interferometry," AIAA Paper No. 93-0631, Jan. 1993.
13. th Asian Congress on Fluid Mechanics, Singapore, 22-26 May 1995.