Aeroelastic Tailoring and Active Aeroelastic Wing Impact on a Lambda Wing Configuration-Reference-Cited by-同舟云学术

Aeroelastic Tailoring and Active Aeroelastic Wing Impact on a Lambda Wing Configuration

Published:2017-01 Issue:1 Volume:54 Page:11-19
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Alyanak Edward J.¹,Pendleton Ed¹

Affiliation:

1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033040

Reference37 articles.

1. Aeroelastic tailoring - Theory, practice, and promise

2. McCullersL. A.NaberhausJ. D.BensingerC. T. “Dynamic Characteristics of Advnaced Filamentary Composite Structures, Volume I—Test Specimen Program,” Air Force Flight Dynamics Labor., U.S. Air Force Systems Command TR AFFDL-TR-73-111, Vol. 1, Wright–Patterson AFB, OH, Sept. 1974.

3. LynchR. W.RogersW. A.BraymenW. W. “Aeroelastic Tailoring of Advanced Composite Structure for Military Aircraft, Volume I—General Study,” Air Force Flight Dynamics Lab., U.S. Air Force Systems Command TR AFFDL-TR-76-100, Vol. 1, Wright–Patterson AFB, OH, April 1977.

4. Aeroelastic Tailoring Studies in Fighter Aircraft Design

5. Aeroelastic Tailoring of Forward Swept Composite Wings

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