Effect of Engine Placement on Aeroelastic Trim and Stability of Flying Wing Aircraft-Reference-Cited by-同舟云学术

Effect of Engine Placement on Aeroelastic Trim and Stability of Flying Wing Aircraft

Published:2012-04-23 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA
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Author:

Mardanpour Pezhman,Hodges Dewey,Neuhart Ryan,Graybeal Nathan

Publisher

American Institute of Aeronautics and Astronautics

Reference20 articles.

1. 2Gyorgy-Falvy, D., Performance analysis of the "Horten IV" Flying Wing. June 1960, Mississippi State University Report:Presented at the8th O.S.T.I.V. Congress, Cologne,Germany.

2. 3Michael H. Love, P.S.Z., Paul A Wieselmann, Harold Youngren, Body Freedom Flutter of High Aspect Ratio FlyingWings, in46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference.April 2005: Austin, Texas.

3. 4Moore, M.D., NASA Puffin Electric Tailsitter VTOL Concept, in10th AIAA Aviation Technology, Integration, and Operations (ATIO)Conference. September 2010, Fort Worth, Texas.

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