On the Calculation of Temperature Distribution and Thermal Stresses in Parts of Aircraft Structures at Supersonic Speeds
- 1 August 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (8) , 575-576
- https://doi.org/10.2514/8.3136
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Temperature Distribution and Thermal Stresses in a Model of a Supersonic WingJournal of the Aeronautical Sciences, 1954
- Stability Derivatives for a Slender Missile with Application to a Wing-Body-Vertical-Tail ConfigurationJournal of the Aeronautical Sciences, 1953