Computation of stability derivatives of spinning missiles using unstructured cartesian meshes

20th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2002, Pages

  Stalnaker, John F ^a   Robinson, Michael A ^a  

^a L 3 Communications Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; COMPUTATIONAL FLUID DYNAMICS; MISSILES;

AERO-DYNAMIC PERFORMANCE; CARTESIAN MESH; CFD CODES; FLIGHT CONFIGURATIONS; SPINNING MISSILES; STABILITY DERIVATIVES; TIME DEPENDENT;

AERODYNAMIC STABILITY;

EID: 85067317429     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-2802     Document Type: Conference Paper

References (11)

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2. Melton, J. E., Berger, M. J., and Aftosmis, M. J., "3D applications of a Cartesian grid Euler method," AIAA Paper 95-0853-CP, Jul. 1993.
3. Aftosmis, M.J., Berger, M.J., Melton, J.E.: "Robust and efficient Cartesian mesh generation for component-based geometry." AIAA Paper 97-0196, Jan. 1997.
4. Aftosmis, M.J., Melton, J.E., and Berger, M.J., "Adaptation and surface modeling for Cartesian mesh methods," AIAA Paper 95-1725-CP, Jun., 1995.
5. Chen, J.P., Ghosh, A.R., Sreenivas, K., and Whitfield, D.L., "Comparison of Computations Using Navier-Stokes Equations in Rotating and Fixed Coordinates for Flow Through Turbomachinery", AIAA Paper No. 97-0878, AIAA 35th Aerospace Sciences Meeting, Reno, NV, Jan. 1997.
6. Oktay, E. and Akay, H.U., "CFD Predictions of Dynamic Derivatives for Missiles", AIAA Paper 2002-0276, AIAA 40th Aerospace Sciences Meeting, Reno, NV, Jan. 2002.
7. Regan, F.J., "Roll Damping Moment Measurements for the Basic Finner at Subsonic and Supersonic Speeds", NAVORD Report 6652, June 1964.
8. Uselton, B.L., and Jenke, L.M., "Experimental Missile Pitch- and Roll-Damping Characteristics at Large Angles of Attack", J. Spacecraft, Vol. 14, No. 4, April 1977.
9. Shantz, I. and Groves, R.T., "Dynamic and Static Stability Measurements of the Basic Finner at Supersonic Speeds", NAVORD Report 4516, Sept. 1960.
10. MacAllister, L.C., "The Aerodynamic Properties of a Simple Non-Rolling Finned Cone-Cylinder Configuration Between Mach Numbers 1.0 and 2.5", Ballistics Research Laboratory, Report 934, May 1955.
11. G. Winn, Dynetics, Inc., private communication.