MDO technology needs in aeroelastic structural design-Reference-Cited by-同舟云学术

MDO technology needs in aeroelastic structural design

Published:1998-08-22 Issue: Volume: Page:
ISSN:
Container-title:7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
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Author:

Hoenlinger H.¹,Krammer J.²,Stettner M.²

Affiliation:

1. German Aerospace Center, Inst. of Aeroelasticity, Goettingen, Germany

2. Daimler-Benz Aerospace AG, Munich, Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-4731

Reference3 articles.

1. Snee, J.M.D., Zimmermann, H.; Schierenbeck, D., Heinz, P.,Simultaneous Stress and Flutter Optimization for the Wing of a Transport Aircraft EquippedWithFourEngines,"Bath,UK 1991.AGARD-R-784. Allwright, S.A.Technical Data Management for Collaborative Multi-disciplineOptimisation," 6* AIAA/NASA/ISSMO Symposium on Multidisci-plinary Analysis and Optimization, Bellevue, Washington,September 1996. AIAA 96-4160. Krammer, J.M.,and Lemmen, G.Integrierte Strukturauslegung mit dem Strukturoptimierungsprogramm LAGRANGE am Beispiel des fliegenden Technologietragers,"DGLR Jahrbuch 1996,pp.625-634.DGLR-JT96-079. Haftka, R.T.Structural Optimization withAeroelastic Constraints: A Survey of US Applications," International Symposium Aeroelasticity,Numberg,Germany, 1991. on

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