Comment on the Stability Derivatives of a Wing-Body-Vertical Tail Configuration
- 1 January 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (1) , 59
- https://doi.org/10.2514/8.2916
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- On Determining the Additional Apparent Mass of a Wing-Body-Vertical-Tail Cross SectionJournal of the Aeronautical Sciences, 1953
- Stress Analysis of Sheet-Stringer Panels with CutoutsJournal 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