Integrated aeroservoelastic wing synthesis by nonlinear programming/approximation concepts
- 1 July 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 15 (4) , 985-993
- https://doi.org/10.2514/3.20933
Abstract
No abstract availableKeywords
This publication has 32 references indexed in Scilit:
- Elements of Structural OptimizationPublished by Springer Nature ,1990
- Integrated aerodynamic/structural design of a sailplane wingJournal of Aircraft, 1988
- Integrated aeroservoelastic tailoring of lifting surfacesJournal of Aircraft, 1988
- Take-Off in Optimum Structural DesignPublished by Springer Nature ,1987
- Control of a forward-swept-wing configuration dominated by flight dynamic/aeroelastic interactionsJournal of Guidance, Control, and Dynamics, 1986
- Multidisciplinary analysis and synthesis - Needs and opportunitiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- On Making Things the Best-Aeronautical Uses of OptimizationJournal of Aircraft, 1982
- Structural synthesis - Its genesis and developmentAIAA Journal, 1981
- Aeroservoelastic EncountersJournal of Aircraft, 1979
- Optimization of flexible wing structures subject to strength and induced drag constraintsAIAA Journal, 1977