Investigations on Missile Configuration Aerodynamic Characteristics for Design Optimization-Reference-Cited by-同舟云学术

Investigations on Missile Configuration Aerodynamic Characteristics for Design Optimization

Published:2014 Issue:4 Volume:57 Page:210-218
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

NGUYEN Nhu-Van,TYAN Maxim,LEE Jae-Woo,BYUN Yung-Hwan

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/57/4/57_210/_pdf

Reference22 articles.

1. 1) Blake, W. B.: Missile DATCOM User's Manual-1997, Fortran 90 Revision, 1998.

2. 2) White, J. T.: An Assessment of Missile Datcom Prediction Accuracy Relative to Generic Body+Wing+Tail Missile Pitch Aerodynamics, AIAA Paper 95-1893-CP, 1995.

3. 3) Abney, E. J. and McDaniel, M. A.: High Angle of Attack Aerodynamic Predictions Using Missile Datcom, AIAA Paper 2005-5086, 2005.

4. 4) Smith, E. H., Hebbar, S. K. and Platzer, M. R.: Aerodynamic Characteristics of a Canard-Controlled Missile at High Angles of Attack, J. Spacecraft Rockets, 31, 5 (1994), pp. 766-772.

5. 5) Riddle, D. B., Hartfield, R. J., Burkhalter, J. E. and Jenkins, R. M.: Genetic-Algorithm Optimization of Liquid-Propellant Missile Systems, J. Spacecraft Rockets, 46, 1 (2009), pp. 151-159.

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