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Volumn 38, Issue 2, 2001, Pages 150-158

Semiempirical prediction of pitch damping moments for configurations with flares

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; DAMPING; METHOD OF MOMENTS; NAVAL WARFARE; TECHNOLOGICAL FORECASTING;

EID: 0035270299     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3688     Document Type: Article
Times cited : (7)

References (18)
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    • edited by P. Zarchan, AIAA, Reston, VA
    • Moore, F. G., Approximate Methods for Weapon Aerodynamics, edited by P. Zarchan, Vol. 186, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2000.
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    • Moore, F.G.1
  • 6
    • 0342720998 scopus 로고    scopus 로고
    • Improvements in Pitch Damping for the Aeroprediction Code with Particular Emphasis on Flare Configurations
    • Dahlgren, VA, April
    • Moore, F. G., and Hymer, T. C., "Improvements in Pitch Damping for the Aeroprediction Code with Particular Emphasis on Flare Configurations," U.S. Naval Surface Warfare Center, Dahlgren Div., Rept. NSWCDD/TR-00/009, Dahlgren, VA, April 2000.
    • (2000) U.S. Naval Surface Warfare Center, Dahlgren Div., Rept. NSWCDD/TR-00/009
    • Moore, F.G.1    Hymer, T.C.2
  • 8
    • 77956966307 scopus 로고
    • Navier-Stokes Predictions of Pitch-Damping for a Family of Flared Projectiles
    • Aberdeen Proving Ground, MD, Oct.
    • Weinacht, P., "Navier-Stokes Predictions of Pitch-Damping for a Family of Flared Projectiles," U.S. Army Research Lab., Rept. ARL-TR-591, Aberdeen Proving Ground, MD, Oct. 1994.
    • (1994) U.S. Army Research Lab., Rept. ARL-TR-591
    • Weinacht, P.1
  • 10
    • 2342466480 scopus 로고
    • Navier-Stokes Predictions of Pitch-Damping for Axisymmetric Shell Using Steady Coming Motion
    • Aberdeen Proving Ground, MD, Sept.
    • Weinacht, P., Sturek, W. B., and Schiff, L. B., Navier-Stokes Predictions of Pitch-Damping for Axisymmetric Shell Using Steady Coming Motion," U.S. Army Research Lab., Rept. ARL-TR-575, Aberdeen Proving Ground, MD, Sept. 1994.
    • (1994) U.S. Army Research Lab., Rept. ARL-TR-575
    • Weinacht, P.1    Sturek, W.B.2    Schiff, L.B.3
  • 11
    • 84983165293 scopus 로고    scopus 로고
    • Prediction of Pitch Damping of Projectiles at Low Supersonic and Transonic Velocities
    • Jan.
    • Weinacht, P., "Prediction of Pitch Damping of Projectiles at Low Supersonic and Transonic Velocities," AIAA Paper 98-0395, Jan. 1998.
    • (1998) AIAA Paper 98-0395
    • Weinacht, P.1
  • 12
    • 2342646565 scopus 로고
    • Transonic Flow-Field Calculation Around Ogive Cylinders by Nonlinear-Linear Stretching Method
    • U.S. Army Missile Command, TR RD-TR-70-12, April 1970; also Jan.
    • Wu, J. M., and Aoyoma, K., "Transonic Flow-Field Calculation Around Ogive Cylinders by Nonlinear-Linear Stretching Method," U.S. Army Missile Command, TR RD-TR-70-12, April 1970; also AIAA Paper 70-189, Jan. 1970.
    • (1970) AIAA Paper 70-189
    • Wu, J.M.1    Aoyoma, K.2
  • 13
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    • Equations, Tables, and Charts for Compressible Flow
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  • 14
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    • Spinner - A Computer Program for Predicting the Aerodynamic Coefficients of Spin Stabilized Projectiles
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    • (1969) General Electric Class 2 Repts.
    • Whyte, R.H.1
  • 17
    • 0343907702 scopus 로고
    • Static Aerodynamics CFD Analysis for 120-mm Hypersonic KE Projectile Design
    • Aberdeen Proving Ground, MD, Sept.
    • Guidos, B. J., "Static Aerodynamics CFD Analysis for 120-mm Hypersonic KE Projectile Design," U.S. Army Research Lab., Rept. ARL-MR-184, Aberdeen Proving Ground, MD, Sept. 1994.
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  • 18
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    • Analysis of Free-Flight Data for the CAN4 Hypersonic Research Projectile
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.