Airworthiness Evaluation of a Scaled Joined-Wing Aircraft-Reference-Cited by-同舟云学术

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Airworthiness Evaluation of a Scaled Joined-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:

Richards Jenner,Aarons Tyler,Garnand-Royo Jeff,Suleman Afzal,Canfield Robert,Woolsey Craig

Publisher

American Institute of Aeronautics and Astronautics

Reference5 articles.

1. Joined-Wing Sensor-Craft Configuration Design

2. The joined wing - An overview

3. 5Richards,J.G,Suleman,A."AeroelasticScalingofUnconventionalJoinedWingConceptforExplorationof Gust Load Response" IFASD ConferenceManuscript,2009, IFASD-2009-2177

Cited by 4 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. Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future;Progress in Aerospace Sciences;2016-11

2. Risks of linear design of joined wings: a non-linear dynamic perspective in the presence of follower forces;CEAS Aeronautical Journal;2014-11-16

3. Nonlinear Aeroelastic Scaled Model Optimization Using Equivalent Static Loads;54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2013-04-05

4. High Fidelity Nonlinear Aeroelastic Analysis for Scaled Vehicle Design;12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2012-09-11

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