Hybrid Wing Body Pressurized Fuselage and Bulkhead Design and Optimization-Reference-Cited by-同舟云学术

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Hybrid Wing Body Pressurized Fuselage and Bulkhead Design and Optimization

Published:2013-04-05 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Mukhopadhyay Vivekanand¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1717

Reference29 articles.

1. Liebeck,R.H."ConfigurationControlDocumentCCD-3:BlendedWingBody,"FinalreportUnderContract NAS1-20275 NASA Langley Research Center, October 1997.

2. Liebeck,R.H.,Page,M.A.,andRawdon,B.K."Blended-Wing-BodySubsonicCommercialTransport," AIAA Paper1998-0438,January1998.

3. Design of the Blended Wing Body Subsonic Transport

4. Structural Concepts Study of Non-circular Fuselage Configurations

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A deformation criterion of pressurized non-circular cross-section cabin and its effects on cruise performance of BWB civil aircraft;Chinese Journal of Aeronautics;2024-06

2. Composite Structure Modeling and Analysis of Advanced Aircraft Fuselage Concepts;AIAA Modeling and Simulation Technologies Conference;2015-06-18

3. Hybrid-Wing-Body Vehicle Composite Fuselage Analysis and Case Study;14th AIAA Aviation Technology, Integration, and Operations Conference;2014-06-13

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