Composite Structure Modeling and Analysis of Advanced Aircraft Fuselage Concepts-Reference-Cited by-同舟云学术

Composite Structure Modeling and Analysis of Advanced Aircraft Fuselage Concepts

Published:2015-06-18 Issue: Volume: Page:
ISSN:
Container-title:AIAA Modeling and Simulation Technologies Conference
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Author:

Mukhopadhyay Vivekanand¹,Sorokach Michael R.¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-3096

Reference21 articles.

1. Blended-wing-body subsonic commercial transport

2. Design of the Blended Wing Body Subsonic Transport

3. Hoffman, K. "Air Vehicle Technology Integration Program (AVTIP), Multi-role Bomber Structural Analysis, AFRL-VAWP-TR-2006-3067, May 2006, Final Report for 14 December 2004-May 2006, AFRL-VA-WP-TR-2006-3067.

4. Analysis, Design, and Optimization of Noncylindrical Fuselage for Blended-Wing-Body Vehicle

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