Aeroelastic, Flight Mechanic, and Handling Qualities of the MOB BWB Configuration-Reference-Cited by-同舟云学术

Aeroelastic, Flight Mechanic, and Handling Qualities of the MOB BWB Configuration

Published:2002-09-04 Issue: Volume: Page:
ISSN:
Container-title:9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
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Author:

Stettner Martin,Voss Ralph

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-5449

Reference15 articles.

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2. Österheld, C.M., Heinze, W., and Horst, P. Preliminary Design of a Blended Wing Body Aircraft using the Design Tool PrADO, Proceedings of the CEAS Conference on Multidisciplinary Aircraft Design and Optimization, Cologne, Germany, June 2001. DGLRReport 2001-005. ISBN 3-932182-21-29.

3. La Rocca, G., Krakers, L., Van Tooren, M. "Development of an ICAD Generative Model for the Blended Wing-Body aircraft.", 9thAIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Atlanta, Georgia, September 2002. AIAA-2002-5447.

4. Qin, N. "Aerodynamic Studies of Blended Wing Body Aircraft," 9thAIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Atlanta, Georgia, September 2002. AIAA-2002-5448.

5. Bråmå, T., Cronemyr, P., and Hansson, E. "Multidisciplinary Optimization of a Composite Wing using an Alternative Approach for Static Aeroelasticity," The International Forum on Aeroelasticity and Structural Dynamics, Manchester, UnitedKingdom, June 1995.

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