Parametric Mesh Deformation and Sensitivity Analysis for Design of a Joined-Wing Aircraft-Reference-Cited by-同舟云学术

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Parametric Mesh Deformation and Sensitivity Analysis for Design of a Joined-Wing Aircraft

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Hur Jiyoung¹,Beran Philip¹,Huttsell Lawrence¹,Snyder Richard¹,Soni Bharat²,Thornburg Hugh³

Affiliation:

1. Air Force Research Laboratory

2. University of Alabama at Birmingham

3. Mississippi State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-116

Reference34 articles.

1. Parametric grid generation applicable to design optimization of centrifugal compressor configurations

2. Yu, T. "CAGD Techniques in Grid Generation," Ph.D Dissertation,Department of Computational Engineering, MississippiState University, December 1995.

3. Koomullil, R. "Flow Simulation System for Generalized Static and Dynamic Grids," Ph.D Dissertation,Department of Aerospace Engineering, Mississippi State University, May 1997.

Cited by 3 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. Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future;Progress in Aerospace Sciences;2016-11

2. Turbine blade temperature transfer using the load surface method;Computer-Aided Design;2007-06

3. Joined-Wing Aeroelastic Design with Geometric Nonlinearity;Journal of Aircraft;2005-07

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