Induced Drag Reduction Using Aeroelastic Tailoring with Adaptive Control Surfaces-Reference-Cited by-同舟云学术

Induced Drag Reduction Using Aeroelastic Tailoring with Adaptive Control Surfaces

Published:2006-01 Issue:1 Volume:43 Page:157-164
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Weisshaar Terrence A.¹,Duke David K.²

Affiliation:

1. Purdue University, West Lafayette, Indiana 47907-1282

2. Lockheed-Martin Company, Fort Worth, Texas 76101

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.12040

Reference32 articles.

1. Aeroelastic tailoring for improved UAV performance

2. 2Duke, D. K. "Induced Drag Reduction Using Aeroelastic Tailoring and Adaptive Control Surfaces," M.S. Thesis, School of Aeronautics and Astronautics,Purdue Univ., West Lafayette,IN, May 2000.

3. Aeroelastic tailoring - Theory, practice, and promise

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