Computational simulations of a three-dimensional high-lift wing

20th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2002, Pages

  Khorrami, Mehdi R ^a   Berkman, Mert E ^b   Li, Fei ^b   Singer, Bart A ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b High Technology Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

LIFT; NAVIER STOKES EQUATIONS; PAINT;

COMPUTATIONAL SIMULATION; FLAP DEFLECTION; HIGH LIFTS; PRESSURE SENSITIVE PAINTS; REYNOLDS - AVERAGED NAVIER-STOKES; ROTATIONAL VELOCITY; SURFACE PRESSURE FIELD; VORTEX BREAKDOWN;

VORTEX FLOW;

EID: 85067320837     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-2804     Document Type: Conference Paper

References (10)

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3. Khorrami, M.R., Singer, B.A., and Takallu, M.A., "Analysis of Flap Side-edge Flow Field for Identification and Modeling of Possible Noise Sources," SAE paper No. 971917. Presented at the 1997 SAE Noise and Vibration Conference and Exposition, Ground Traverse, Michigan, May 1997.
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7. Thomas, J., Krist, S., and Anderson, W., "Navier- Stokes Computations of Vortical Flows over Low Aspect-Ratio Wings," AIAA J., Vol. 28, No.2, pp. 205-212, 1990.
8. Spalart, P.R. and Allmaras, S.R., "A One-Equation Turbulence Model for Aerodynamics Flows," AIAA Paper 92-0439, 1992.
9. Dacles-Mariani, J., Rogers, S., Kwak, D., Zilliac, G., and Chow, J., "A Computational Study of Wingtip Vortex Flowfield," AIAA Paper 93-3010, July 1993.
10. Khorrami, M. R., Li, F., and Choudhari, M., "A Novel Approach for Reducing Rotor Tip-Clearance Induced Noise in Turbofan Engines,"AIAA Paper 2001-2148 (also to appear in July 2002 issue of AIAA J.), May 2001.