Alternative Approximations for Integrated Control/Structure Aeroservoelastic Synthesis
- 1 June 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (6) , 1100-1108
- https://doi.org/10.2514/3.49052
Abstract
No abstract availableThis publication has 20 references indexed in Scilit:
- Studies in integrated aeroservoelastic optimization of actively controlled composite wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Towards integrated multidisciplinary synthesis of actively controlled fiber composite wingsJournal of Aircraft, 1990
- Reduced-order aeroelastic models via dynamic residualizationJournal of Aircraft, 1990
- Exploratory design studies using an integrated multidisciplinary synthesis capability for actively controlled composite wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Elements of Structural OptimizationPublished by Springer Nature ,1990
- Approximations to eigenvalues of modified general matricesComputers & Structures, 1988
- Integrated aeroservoelastic tailoring of lifting surfacesJournal of Aircraft, 1988
- Aeroelastic tailoring - Theory, practice, and promiseJournal of Aircraft, 1986
- Multidisciplinary analysis and synthesis - Needs and opportunitiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Aeroservoelastic EncountersJournal of Aircraft, 1979