Evaluation of the Inertia Coefficients of the Cross Section of a Slender Body
Author:
Affiliation:
1. Harvard University, Cambridge, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.3063
Reference11 articles.
1. Stability Derivatives for a Slender Missile with Application to a Wing-Body-Vertical-Tail Configuration
2. SUPERSONIC FLOW PAST SLENDER POINTED BODIES
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