Optimal External Configuration Design of Unguided Missiles
Author:
Affiliation:
1. Defense Industries Research and Development Institute, Ankara 06, Turkey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3328
Reference4 articles.
1. Parametric aerodynamic design of spinning finned projectiles using amatrix interpolation method
2. Pierre, D. A., Optimization Theory with Applications, Dover, New York, 1986, pp.264-366.
3. Nielsen, J. N., Missile Aerodynamics, Nielsen Engineeringand Research, Inc., Mountain View,CA, 1988, pp.349-431.
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