Measurement and simulation of wake deceleration

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Hoffenberg, R ^a   Sullivan, J P ^a  

^a Purdue University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; FIGHTER AIRCRAFT; NAVIER STOKES EQUATIONS; PRESSURE GRADIENT; TURBULENCE MODELS;

ADVERSE PRESSURE GRADIENT; AIRCRAFT PERFORMANCE; COMPUTATIONAL INVESTIGATION; DIFFUSER ANGLE; HIGH LIFT SYSTEM; MEASUREMENT AND SIMULATION; TURBULENT WAKE; TWO-DIMENSIONAL DIFFUSER;

WAKES;

EID: 84982317969     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (26)

1. Cornish, J. J. "Some Aerodynamic and Operational Problems of STOL Aircraft with Boundary-Layer Control," Journal of Aircraft, Vol. 2, Feb. 1965, pp. 78-86.
2. Drela, M. "Newton Solution of Coupled Viscous/lnviscid Multielement Airfoil Flows," AIAA Paper 90-1470, 1990.
3. FLUENT User's Guide, vol. 1, Release 4. 4, Fluent inc., August 1996.
4. Garner, P. L., Meredith, P. T., and Stoner, R. C. "Areas for Future CFD Development as Illustrated by Transport Aircraft Applications," AIAA Paper No. 91-1527-CP, 1991.
5. Hill, P. G., Schaub, U. W., and Senoo, Y. "Turbulent Wakes in Pressure Gradients," Journal of Applied Mechanics, Vol. 30, Dec. 1963, pp. 518-524.
6. Hoffenberg, R., Sullivan, J. P., and Schneider, S. P., "Wake Measurements in a Strong Adverse Pressure Gradient," AIAA Paper 95-1912, 1995.
7. Hoffenberg, R., and Sullivan, J. P., "Simulation of High-Lift Wake Behavior," AIAA Paper 97-0718, 1997.
8. Johnston, L. J., and Stolcis, L., "Prediction of the High-Lift Performance of Multi-Element Airfoils Using an Unstructured Navier-Stokes Solver," AGARD CP-515, Sec. 13, 1992.
9. Kato, M. And Launder, B. E., 'The Modeling of Turbulent Flow Around Stationary and Vibrating Square Cylinders," Proc. 9th Symposium Turbulent Shear Flows, Kyoto, No. 10-4, 1993.
10. Lin, J. Optimization of an Advanced Design Three Element Airfoil at High Reynolds Numbers," AIAA Paper 95-1858, 1995.
11. Lynch, F. T., "Experimental Necessities for Subsonic Transport Configuration Development," AIAA Paper 92-0158, 1992.
12. Mack, M. D. and McMasters, J. H. "High Reynolds Number Testing in Support of Transport Airplane Development," AIAA Paper 92-3982, 1992.
13. McMasters, J. H., Roberts, W. H., Payne, F. M., Sandford, M. C., and Durham, M. "Recent Air-Freon Tests of a Transport Airplane in High-Lift Configurations," AIAA Paper 88-2034, 1988.
14. Menter, F. R. "Zonal Two-Equation k-ω Turbulence Models for Aerodynamic Flows," AIAA Paper 93-2906, 1993.
15. Menter, F. R., "Improved Two-Equation k-ω Turbulence Models for Aerodynamic Flows," NASA Report TM-103975, Oct. 1992.
16. Meredith, P. T., "Viscous Phenomena Affecting High-Lift Systems and Suggestions for Future CFD Development," AGARD CP-515, Sec. 19, 1992.
17. Petrov, A. V. "Certain Types of Separated Flow Over Slotted Wings," Fluid Mechanics -Soviet Research, Vol. 7., Sept. /Oct. 1978, pp. 80-89.
18. Reneau, L. R., Johnston, J. P., and Kline, S. J. "Performance of Straight, Two-Dimensional Diffusers," ASME Journal of Basic Engineering, March 1967, pp. 141-160.
19. Roos, F. W. "Experimental Studies of Wake Retardation in a Simulated High-Lift-System Flow Field," AIAA Paper No. 97-1813, July, 1997.
20. Schneider, S., Campbell, B., Bucci, G., and Sullivan, J. "An Experimental Simulation of Flap Flow on Multi-element Airfoils at High Reynolds Number," AIAA Paper 94-2613, 1994.
21. Smith, A. M. O. "High-lift aerodynamics," Journal of Aircraft, Vol. 12, June 1975, pp. 501-530
22. Spalart, P. Private Communication.
23. Tulapurkara, E. G., Ramjee, V., and George, J. "Development of a Bluff Body Wake Under the Combined Influence of Curvature and Pressure Gradient," Experiments in Fluids, Vol. 18, March 1995, pp. 311-318.
24. van Dam, C. P., Los, S. M., Miley, S. J., Yip, L. P., Banks, D. W., Roback, V. E., Bertelrud, A. "Analysis of In-Flight Boundary-Layer State Measurements on a Subsonic Transport Wing in High-Lift Configuration," AIAA Paper 95-3911, 1995.
25. Valarezo, W. O., "High-Lift Testing at High Reynolds Numbers," AIAA Paper 92-3986, 1992.
26. Wygnanski, I., Champagne, F., and Marasli, B. "On the Large-Scale Structures in TwoDimensional, Small-Deficit, Turbulent Wakes," Journal of Fluid Mechanics, Vol. 168, July 1986, pp. 31-71.