An aerodynamic analysis of a spinning missile with dithering canards

20th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2002, Pages

  Nygaard, Tor A ^a   Meakin, Robert L ^a  

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; DATABASE SYSTEMS; MISSILES; VISCOUS FLOW;

ACCURATE PREDICTION; AERODYNAMIC ANALYSIS; AERODYNAMIC DATABASE; ANALYTICAL METHOD; GRID RESOLUTION; ROLLING AIRFRAME MISSILES; SPINNING MISSILES; STRUCTURED GRID;

NAVIER STOKES EQUATIONS;

EID: 85067320773     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-2799     Document Type: Conference Paper

References (6)

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2. Meakin, R., "Automatic Off-Body Grid Generation for Domains of Arbitrary Size," AIAA-2001-2536, 15th AIAA Computational Fluid Dynamics Conf., June 2001, Anaheim, CA.
3. Meakin, R., "Adaptive Spatial Partitioning and Refinement for Overset Structured Grids" Comput. Methods Appl. Mech. Engrg., Vol. 189 (2000), 1077-1117.
4. Chan, W., "The OVERGRID Interface for Computational Simulations on Overset Grids" AIAA Paper 2002-3188, 32nd AIAA Fluid Dynamics Conference, St.~Louis, Missouri, June, 2002.
5. Chan, W., Meakin, R., and Potsdam, M., "CHSSI Software for Geometrically Complex Unsteady Aerodynamic Applications," AIAA 2001-0539, AIAA 39th Aerosciences Meeting and Exhibit, January, 2001, Reno, NV.
6. Buning, P. G., Jespersen, D. C., Pulliam, T.H., Chan, W. M., Slotnick, J. P., Krist, S. E. and Renze, K. J., "OVERFLOW User's Manual," Version 1.8, NASA Langley Research Center, 1998.