Aerodynamic investigation of twist and cant angles for joined wing transport aircraft-Reference-Cited by-同舟云学术

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Aerodynamic investigation of twist and cant angles for joined wing transport aircraft

Published:1997-01-06 Issue: Volume: Page:
ISSN:
Container-title:35th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Bagwill Tracy¹,Selberg Bruce²,Bagwill Tracy¹,Selberg Bruce²

Affiliation:

1. Boeing Co., Seattle, WA

2. Missouri-Rolla, Univ., Rolla

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-37

Reference15 articles.

1. Knight,M.andNoyes,R. W."Wind TunnelTest on a Series of Biplane Wing Models, Part I. Effects of Changes in Stagger and Gap,"NACA TN-130, 1929.

Cited by 7 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. Aerodynamic Interference Significance Analysis of Two-Dimensional Front Wing and Rear Wing Airfoils with Stagger and Gap Variations;Journal of Aerospace Engineering;2019-11

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

3. Conceptual design of a nonplanar wing airliner;Aircraft Engineering and Aerospace Technology;2016-07-04

4. Clean Sheet Design;Advanced Aircraft Design;2013-05-27

5. Aeroelastic Tailoring of Joined-Wing Configurations;43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2002-04-22

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