Evaluation of the Inertia Coefficients of the Cross Section of a Slender Body
- 1 June 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (6) , 424-427
- https://doi.org/10.2514/8.3063
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- On Determining the Additional Apparent Mass of a Wing-Body-Vertical-Tail Cross SectionJournal of the Aeronautical Sciences, 1953
- Stability Derivatives for a Slender Missile with Application to a Wing-Body-Vertical-Tail ConfigurationJournal of the Aeronautical Sciences, 1953
- SUPERSONIC FLOW PAST SLENDER POINTED BODIESThe Quarterly Journal of Mechanics and Applied Mathematics, 1949