Navier-Stokes predictions of the individual components of the pitch-damping sum

Journal of Spacecraft and Rockets

Volumn 35, Issue 5, 1998, Pages 598-605

  Weinacht, Paul ^a,b  

^a U S ARMY RESEARCH LABORATORY   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; DAMPING; NAVIER STOKES EQUATIONS; STEADY FLOW;

PITCH-DAMPING COEFFICIENT SUM;

AERODYNAMICS;

EID: 0032158293     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3390     Document Type: Article

References (16)

1. Schiff, L. B., "Nonlinear Aerodynamics of Bodies in Coning Motion," AIAA Journal, Vol. 10, No. 11, 1972, pp. 1517-1522.
2. Agarwal, R., and Rakich, J. V., "Computation of Supersonic Laminar Viscous Flow Past a Pointed Cone at Angle of Attack in Spinning and Coning Motion," AIAA Paper 78-1211, July 1978.
3. Lin, T. C., "A Numerical Study of the Aerodynamics of a Reentry Vehicle in Steady Coning Motion," AIAA Paper 78-1358, Aug. 1978.
4. Weinacht, P., and Sturek, W. B., "Navier-Stokes Predictions of Pitch Damping for Finned Projectiles Using Steady Coning Motion," Proceedings of the AIAA 8th Applied Aerodynamics Conference, AIAA, Washington, DC, 1990, pp. 632-642 (AIAA Paper 90-3088, Aug. 1990).
5. Weinacht, P., Sturek, W. B., and Schiff, L. B., "Navier-Stokes Predictions of Pitch-Damping for Axisymmetric Shell Using Steady Coning Motion," Proceedings of the 1991 Atmospheric Flight Mechanics Conference, AIAA, Washington, DC, 1991, pp. 89-100 (AIAA Paper 91-2855, Aug. 1991).
6. Weinacht, P., "Navier-Stokes Predictions of Pitch-Damping for a Family of Flared Projectiles," Proceedings of the 9th Applied Aerodynamics Conference, Vol. 2, AIAA, Washington, DC, 1991, pp. 1025-1034 (AIAA Paper 91-3339, Sept. 1991).
7. Weinacht, P., "Navier-Stokes Predictions of the Individual Components of the Pitch-Damping Coefficient Sum," Proceedings of the 1995 Atmospheric Flight Mechanics Conference, AIAA, Washington, DC, 1995, pp. 291-301 (AIAA Paper 95-3458, Aug. 1995).
8. Weinacht, P., "Prediction of Pitch-Damping Aerodynamic Derivatives Using Navier-Stokes Computational Techniques," Ph.D. Dissertation, Dept. of Mechanical Engineering, Univ. of Delaware, Newark, DE, Spring 1996.
9. Qin, N., Ludlow, D. K., Shaw, S. T., Edwards, J. A., and Dupuis, A., "Calculation of Pitch Damping Coefficients for Projectiles," AIAA Paper 97-0405, Jan. 1997.
10. Murphy, C. H., "Free Flight Motion of Symmetric Missiles," U.S. Army Ballistic Research Lab., Rept. 1216, Aberdeen Proving Ground, MD, July 1963.
11. Baldwin, B. S., and Lomax, H., "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows," AIAA Paper 78-257, Jan. 1978.
12. Schiff, L. B., and Steger, J. L., "Numerical Simulation of Steady Supersonic Viscous Flow," AIAA Journal, Vol. 18, No. 12, 1980, pp. 1421-1430.
13. Beam, R., and Warming, R. F., "An Implicit Factored Scheme for the Compressible Navier-Stokes Equations," AIAA Journal, Vol. 16, No. 4, 1978, pp. 393-402.
14. Rai, M. M., and Chaussee, D. S., "New Implicit Boundary Procedure: Theory and Applications," AIAA Paper 83-0123, Jan. 1983.
15. Sturek, W. B., and Schiff, L. B., "Computations of the Magnus Effect for Slender Bodies in Supersonic Flight," Proceedings of the AIAA Atmospheric Flight Mechanics Conference, AIAA, New York, 1980, pp. 260-280 (AIAA Paper 80-1586, Aug. 1980).
16. Murphy, C. H., and Schmidt, L. E., "The Effect of Length on the Aerodynamics Characteristics of Bodies of Revolution in Supersonic Flight," U.S. Army Ballistic Research Lab., Rept. 876, Aberdeen Proving Ground, MD, Aug. 1953.