Structural optimization of lifting surfaces with divergence and control reversal constraints
- 1 September 1989
- journal article
- Published by Springer Nature in Structural and Multidisciplinary Optimization
- Vol. 1 (3) , 153-161
- https://doi.org/10.1007/bf01637335
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Integrated aerodynamic/structural design of a sailplane wingJournal of Aircraft, 1988
- Aeroelastic tailoring for oblique wing lateral trimPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Aeroelastic tailoring - Theory, practice, and promiseJournal of Aircraft, 1986
- NEWSUMT-A: A General Purpose Program for Constrained Optimization Using Constraint ApproximationsJournal of Mechanical Design, 1985
- Divergence speed degradation of forward-swept wings with damaged composite skinJournal of Aircraft, 1984
- Dynamic stability of flexible forward swept wing aircraftJournal of Aircraft, 1983
- Forward Swept Wing Static AeroelasticityPublished by Defense Technical Information Center (DTIC) ,1979
- Aeroelastic Stability and Performance Characteristics of Aircraft with Advanced Composite Sweptforward Wing StructuresPublished by Defense Technical Information Center (DTIC) ,1978
- An efficient structural resizing procedure for meeting static aeroelastic design objectivesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Optimal Aeroelastic Design of an Oblique Wing StructureJournal of Aircraft, 1976