Direct calculation of three-dimensional indicial lift response using computational fluid dynamics

Journal of Aircraft

Volumn 34, Issue 4, 1997, Pages 465-471

  Singh, Rajneesh ^a,b,c   Baeder, James D ^a,b,c  

^a UNIVERSITY OF MARYLAND   (United States)

^b UNIVERSITY OF MARYLAND   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SOFTWARE; LIFT; UNSTEADY FLOW;

EULER SOLVER; INDICIAL LIFT RESPONSE;

WINGS;

EID: 0031189057     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2214     Document Type: Article

References (8)

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3. Leishman, J. G., "Indicial Lift Approximations for Two-Dimensional Subsonic Flow as Obtained from Oscillatory Measurements," Journal of Aircraft, Vol. 30, No. 3, 1993, pp. 340-351.
4. Leishman, J. G., "Validation of Approximate Indicial Aerodynamic Functions for Two-Dimensional Subsonic Flow," Journal of Aircraft, Vol. 25, No. 10, 1988, pp. 914-922.
5. Lesieuture, D. J., Reisenthel, P. H., and Dillenius, M. F. E., "A Practical Approach for Calculating Aerodynamic Indicial Functions with a Navier-Stokes Solver," AIAA Paper 94-0059, Jan. 1994.
6. 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, 1993, pp. 2371-2378.
7. Parameswaran, V. and Baeder, J. D., "Indicial Aerodynamics in Compressible Flow-Direct Computational Fluid Dynamic Calculations," Journal of Aircraft, Vol. 34, No. 1, 1997, pp. 131-133.
8. Khanna, H., and Baeder, J. D., "Coupled Wake/CFD Solutions for Rotors in Hover," 52nd Annual Forum of the American Helicopter Society, Washington DC, June 1996.