Prediction of aerodynamic characteristics of unconventional missile configurations using component build-up techniques
- 6 January 1986
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Application of slender body theory to missiles with arbitrary shape cross sectionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Aerodynamic prediction rationale for advanced arbitrarily shaped missile conceptsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Component aerodynamic characteristics of banked cruciform missiles with arbitrary control deflectionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977