The direct calculation of indicial lift response of a wing using computational fluid dynamics

14th Applied Aerodynamics Conference

Volumn , Issue , 1996, Pages 1041-1050

  Singh, Rajneesh ^a   Baeder, James D ^a  

^a UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; COMPUTATIONAL FLUID DYNAMICS;

ANALYTICAL RESULTS; DIRECT CALCULATION; FLOW FEATURES; NEW APPROACHES; NUMERICAL INSTABILITY; NUMERICAL RESULTS; RECTANGULAR WINGS; STEP CHANGES;

PLANFORMS;

EID: 84889527755     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-2508     Document Type: Conference Paper

References (7)

1. Bisplinghoff R.L., Ashley, H., and Halfman, R.L., "Aeroelasticity," Addison-Wesley Publishing Co., Reading, Mass., 1955
2. Lomax, H., "Indicial Aerodynamics," AGARD Manual of Aeroelasticity, Pt. II, November 1960, Chapter 6
3. Leishman, J.G., "Validation of Approximate Indicial Aerodynamic Functions for Two-Dimensional Flow," Journal of Aircraft, Vol. 25, No. 10, 1986.
4. Lesieuture, D.J., Reisenthel, P.H., and Dille-nius, M.F.E., "A Practical Approach for Cal­culating Aerodynamic Indicial Functions with a Navier-Stoles Solver," 32nd Aerospace Sci­ences Meeting and Exhibit, Reno, NV, No. AIAA 94-0059, January 1994.
5. Srinivasan, G.R. and Baeder, J.D., "TURNS: A Free Wake Euler/ Navier-Stokes Numerical Method for Helicopter Rotors," AIAA Journal, Vol. 31 No. 5, May 1993.
6. Parameshwaran, V., "Concepts for Reduction of Blade Vortex Interaction Noise and the Use of CFD to Determine Indicial and Gust Responses of an Airfoil in Compressible Flow," MS Scholarly paper, Department of Aerospace Engineering, University of Maryland, 1995
7. Leishman, J.G., "Indicial Lift Approximations for Two-Dimensional Subsonic Flow as Ob­tained from Oscillatory Measurements," Journal of Aircraft, Vol. 30, No. 3, 1993