Aeroelastic tailoring of a forward swept wing and comparisons with three equivalent aft swept wings-Reference-Cited by-同舟云学术

Aeroelastic tailoring of a forward swept wing and comparisons with three equivalent aft swept wings

Published:1980-05-12 Issue: Volume: Page:
ISSN:
Container-title:21st Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

TRIPLETT W.¹

Affiliation:

1. McDonnell Aircraft Co., St. Louis, Mo.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1980-794

Reference9 articles.

1. Divergence elimination with advanced composites

2. Divergence of forward swept composite wings

3. An Efficient Structural Resizing Procedure for Meeting Static Aeroelastic Design Objectives

4. Woodward, F. A., and Hague, D. S. "A Computer Program for the Aerodynamic Analysis and Design of Wing-Body-Tail Combinations at Subsonic and Supersonic Speeds," General Dynamics Report ERR-FW-867, Vols. I and 11,Sep 1970.

Cited by 8 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. Tailored Wing Design and Panel Case Study;Commercial Aircraft Composite Technology;2016

2. Optimum design of composite plate wings for aeroelastic characteristics using lamination parameters;Computers & Structures;2007-02

3. Research on Optimum Design of Composite Plate Wings for Aeroelastic Characteristics Using Lamination Parameters (The Second Report)-Optimum Design of Composite Plate Wings for Flutter and Divergence Characteristics-;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2003

4. Research on Optimum Design of Composite Plate Wings for Aeroelastic Characteristics Using Lamination Parameters (The First Report)-flutter and Divergence Characteristics of Composite Plate Wings-;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2003

5. Aeroelastic tailoring - Theory, practice, and promise;Journal of Aircraft;1986-01