Numerical simulation of a spinning missile with dithering canards using unstructured grids

Journal of Spacecraft and Rockets

Volumn 41, Issue 2, 2004, Pages 248-256

  Blades, Eric L ^a,b   Marcum, David L ^a,b  

^a MISSISSIPPI STATE UNIVERSITY   (United States)

^b Engineering Research Center   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; ENTHALPY; OPTICAL RESOLVING POWER; TENSORS; VECTORS; VISCOSITY; VISCOUS FLOW;

CARTESIAN COMPONENTS; FLUID DENSITY; MACH NUMBER; ROLLING MOMENT;

MISSILES;

EID: 2342477825     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.9197     Document Type: Article

References (11)

1. Murman, S. M., Aftosmis, M. J., and Berger, M. J., "Numerical Simulation of Rolling Airframes Using a Multilevel Cartesian Method," Journal of Spacecraft and Rockets (to be published).
2. Hall, L. H., "Chimera Moving Body Methodology for Rolling Airframe Missile Simulation with Dithering Canards," AIAA Paper 2002-2801, June 2002.
3. Nygaard, T. A., and Meakin, R. L., "Aerodynamic Analysis of a Spinning Missile with Dithering Canards," Journal of Spacecraft and Rockets (to be published); also AIAA Paper 2002-2799, June 2002.
4. Nygaard, T. A., and Meakin, R. L., "Aerodynamic Analysis of a Spinning Missile with Dithering Canards," Journal of Spacecraft and Rockets (to be published); also AIAA Paper 2002-2799, June 2002.
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8. Roe, P., "Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes," Journal of Computational Physics, Vol. 43, No. 2, 1981, pp. 357-372.
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11. Defensive Missile Wind Tunnel Test for the Validation and Verification of CFD Codes," Dynetics, Technical Rept., Huntsville, AL, Jan. 2002.