CFD Analysis of Aerodynamic Interference Between a Delta Wing and a Hemisphere-Cylinder-Reference-Cited by-同舟云学术

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CFD Analysis of Aerodynamic Interference Between a Delta Wing and a Hemisphere-Cylinder

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

Author:

Kitamura Keiichi¹,Nakamura Tetsuya¹,Men'shov Igor¹,Nakamura Yoshiaki¹

Affiliation:

1. Nagoya Univ.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-1378

Reference14 articles.

1. Future reusable launch vehicles in europe: the FLTP (Future Launchers Technologies Programme)

2. Hyper-X stage separation--simulation development and results

3. Euler and Navier-Stokes Simulations of Two-Stage Hypersonic Vehicle Longitudinal Motions

4. Waverider Aerodynamics and Preliminary Design for Two-Stage-to-Orbit Missions, Part 1

Cited by 2 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. Shock/Shock and Shock/Boundary-Layer Interactions in Two-Body Configurations;35th AIAA Fluid Dynamics Conference and Exhibit;2005-06-06

2. A Device for Reduction of Heat Flux Produced by Hypersonic Shock Interference;34th AIAA Fluid Dynamics Conference and Exhibit;2004-06-19

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