A computational study of the aerodynamics of a body immersed in a supersonic wake-Reference-Cited by-同舟云学术

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A computational study of the aerodynamics of a body immersed in a supersonic wake

Published:1994-08-01 Issue: Volume: Page:
ISSN:
Container-title:19th Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

Ober Curtis¹,Lamb J.¹,Kiehne Thomas¹

Affiliation:

1. Texas, Univ., Austin

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-3519

Reference20 articles.

1. Observations of turbulent reattachment behind an axisymmetric downstream-facing step in supersonic flow.

2. M. Beheim, "Flow in the Base Region of Axisymmetric and Two-Dimensional Configurations," Tech. Rep. NASA TR R-77, NASA, 1961.

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. A study of unsteady hypersonic segmented projectile aerodynamics;14th Computational Fluid Dynamics Conference;1999-08-22

2. Aerodynamics of a body immersed in a supersonic wake - A computational study;Journal of Spacecraft and Rockets;1995-11

3. A computational study of the aerodynamics of a body immersed in a supersonic wake;19th Atmospheric Flight Mechanics Conference;1994-08-01

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