Optimum structural sizing for gust-induced response
- 1 April 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 26 (4) , 395-397
- https://doi.org/10.2514/3.45773
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Optimum structural sizing for gust induced responsePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Automated structural synthesis for nondeterministic loadsComputer Methods in Applied Mechanics and Engineering, 1986
- Prediction of range and endurance of jet aircraft at constant altitudeJournal of Aircraft, 1981
- Dynamic gust, landing, and taxi loads determination in the design ofthe L-1011.Journal of Aircraft, 1973
- Performance and stability of hypervelocity aircraft flying on a minor circleProgress in Aerospace Sciences, 1972
- Longitudinal Dynamics of a Lifting Vehicle in Orbital FlightJournal of the Aerospace Sciences, 1961