Multidisciplinary Approach to Assessing Actuation Power of a Hybrid Wing

Multidisciplinary Approach to Assessing Actuation Power of a Hybrid Wing–Body

Published:2016-07 Issue:4 Volume:53 Page:900-913
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Garmendia Daniel C.¹,Chakraborty Imon¹,Mavris Dimitri N.¹

Affiliation:

1. Georgia Institute of Technology, Atlanta, Georgia 30332

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033390

Reference30 articles.

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2. Design of the Blended Wing Body Subsonic Transport

3. Aerodynamic design challenges of the Blended-Wing-Body subsonic transport

4. BonetJ. T.SchellengerH. G.RawdonB. K.ElmerK. R.WakayamaS. R.BrownD. L.GuoY. “Environmentally Responsible Aviation (ERA) Project – N+2 Advanced Vehicle Concepts Study and Conceptual Design of Subscale Test Vehicle (STV)—Final Report,” Boeing Research and Technology, TR, Huntington Beach, CA, 2011.

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