On Determining the Additional Apparent Mass of a Wing-Body-Vertical-Tail Cross Section
- 1 December 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (12) , 856-857
- https://doi.org/10.2514/8.2886
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Stability Derivatives for a Slender Missile with Application to a Wing-Body-Vertical-Tail ConfigurationJournal of the Aeronautical Sciences, 1953