Dynamic gust, landing, and taxi loads determination in the design ofthe L-1011.
- 1 August 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 10 (8) , 459-467
- https://doi.org/10.2514/3.44383
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Application of Advanced Methods to Design Loads Determination for the L-1011 TransportJournal of Aircraft, 1973