A Rapid Synthesis Method to Develop Conceptual Design Transonic Wing Lofts-Reference-Cited by-同舟云学术

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A Rapid Synthesis Method to Develop Conceptual Design Transonic Wing Lofts

Published:2010-06-26 Issue: Volume: Page:
ISSN:
Container-title:13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference
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Author:

Donovan Shane¹,Takahashi Timothy¹

Affiliation:

1. Northrop Grumman Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-9025

Reference10 articles.

1. Marx, W.J., Mavris, D.N. and Schrage, D.P. "Integrating Design and Manufacturing for a High Speed Civil Transport Wing,"ICAS 94-1084,1994.

2. McCullers, L.A., FLOPS: Aircraft Configuration Optimization. NASACP-2327,1984

3. Synder, C, et.al. "Propulsion Investigation for Zero andnear ZeroEmissionsAircraft,"NASATM-2009-215487,2009.

4. Hecks, K.G. "TheHigh Speed Shape."Flight International.2 January1964.

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