A Design Study Employing Aeroelastic Tailoring and an Active Aeroelastic Wing Design Approach on a Tailless Lambda Wing Configuration-Reference-Cited by-同舟云学术

A Design Study Employing Aeroelastic Tailoring and an Active Aeroelastic Wing Design Approach on a Tailless Lambda Wing Configuration

Published:2014-06-13 Issue: Volume: Page:
ISSN:
Container-title:15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
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Author:

Alyanak Edward J.¹,Pendleton Edmund¹

Affiliation:

1. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-3158

Reference18 articles.

1. Aeroelastic tailoring - Theory, practice, and promise

2. McCullers L. A., Naberhaus J. D., Bensinger C. T. "Dynamic Characteristics of Advnaced Filamentary Composite Structures, VolumeI- Test Specimen Program," Air Force Flight Dynamics Laboratory, Air Force Systems Command, Wright-Patterson Air Force Base,OH, Technical Report AFFDL-TR-73-111, Volume 1,September 1974.

3. Ply-orientation as a variable in multidisciplinary optimization

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