Evaluation of B-52 structural response to random turbulence with stability augmentation systems.
- 1 November 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 4 (6) , 507-512
- https://doi.org/10.2514/3.43878
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Summary of flight load environmental data taken on b-52 fleet aircraftJournal of Aircraft, 1965
- Cumulative Damage in FatigueJournal of Applied Mechanics, 1945