Experimental Investigation of the Low-Speed Aerodynamic Characteristics of a 5.8-Percent Scale Hybrid Wing Body Configuration-Reference-Cited by-同舟云学术

Experimental Investigation of the Low-Speed Aerodynamic Characteristics of a 5.8-Percent Scale Hybrid Wing Body Configuration

Published:2012-06-25 Issue: Volume: Page:
ISSN:
Container-title:30th AIAA Applied Aerodynamics Conference
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Author:

Gatlin Gregory¹,Vicroy Dan¹,Carter Melissa¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2669

Reference14 articles.

1. 1Dowling,A.andGreitzer,E."TheSilentAircraftInitiative-Overview,"AIAA-2007-0452,January2007.

2. 2Collier, F., Thomas, R., Burley, C., Nickol, C., Lee, M., and Tong, M. "Real Solutions For Environmental Challenges Facing Aviation," ICAS-2010-1.6.1.

3. Technology Assessment of NASA Environmentally Responsible Aviation Advanced Vehicle Concepts

4. 4Nickol,C.andMcCullers,A."HybridWingBodyConfigurationSystemsStudies,"AIAA-2009-931.

5. 5Kimmel, W. "Systems Analysis Approach for the NASA Environmentally Responsible Aviation Project," AIAA-2011-3528.

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