The aerodynamic design of the wing-fuselage for a near-sonic transport-Reference-Cited by-同舟云学术

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The aerodynamic design of the wing-fuselage for a near-sonic transport

Published:2002-01-14 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA Aerospace Sciences Meeting & Exhibit
language:
Short-container-title:

Author:

Haines B.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-517

Reference4 articles.

1. 7-0.0 0.2 0.4 x/c0.6

2. on 3DWing and onEquivalent 2D Section ,n1.09 1.06 !1>131.15 1-13 1.10

3. 2 0.4 0.6 0-8-1.0 Fig 11 Development of Shock Strengthand

Cited by 4 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. Drag Reduction of a Near-Sonic Airplane by Using Computational Fluid Dynamics;AIAA Journal;2005-09

2. Aerodynamic Optimization of NEXST-1 SST Model at Near-Sonic Regime;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

3. Aerodynamic Optimization of Supersonic Transport at Near-Sonic Regime;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2003

4. Transonic Design of SST;IUTAM Symposium Transsonicum IV;2003

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