Study of a global design space exploration method for aerospace vehicles-Reference-Cited by-同舟云学术

Study of a global design space exploration method for aerospace vehicles

Published:2000-09-06 Issue: Volume: Page:
ISSN:
Container-title:8th Symposium on Multidisciplinary Analysis and Optimization
language:
Short-container-title:

Author:

Baker Chuck,Watson Layne,Grossman Bernard,Haftka Raphael,Mason William

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-4763

Reference13 articles.

1. C.A. Baker, B. Grossman, R.T. Haftka, W.H. Mason, and L.T. Watson, HSCT configuration design space exploration using aerodynamic response surface approximations, inProceedings of 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Saint Louis, MO, 1998, pp.769-777.

2. H. Carlson, R. Mack, and R. Barger, Estimation of attainable leading edge thrust for wings at subsonic and supersonic speeds, Technical Report NASA TP-1500, 1979.

3. H. Carlson and D. Miller, Numerical methods for the design and analysis of wings at supersonic speeds, Technical Report NASA TN D7713, 1974.

4. R. Harris Jr, An analysis and correlation of aircraft wave drag, Technical Report NASA TM X947, 1964.

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