Design of the Blended Wing Body Subsonic Transport

R. H. Liebeck

doi:10.2514/1.9084

journal article Jan 01, 2004

Design of the Blended Wing Body Subsonic Transport

R. H. Liebeck

Journal of Aircraft Vol. 41 No. 1 pp. 10-25 · American Institute of Aeronautics and Astronautics (AIAA)

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References

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5Rodriguez, D. L. "A Multidisciplinary Optimization Method for Designing Boundary Layer Ingesting Inlets," Ph.D. Dissertation,Dept. of Aeronautics and Astronautics, Stanford Univ., Stanford, CA,Jan. 2001. 10.2514/6.2002-5665

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Citations

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References

Details

Published: Jan 01, 2004
Vol/Issue: 41(1)
Pages: 10-25

Authors

R

R. H. Liebeck

The Boeing Company, Huntington Beach, California 92647

Cite This Article

R. H. Liebeck (2004). Design of the Blended Wing Body Subsonic Transport. Journal of Aircraft, 41(1), 10-25. https://doi.org/10.2514/1.9084

Design of the Blended Wing Body Subsonic Transport

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