Effects of a Swirling Flow Motion on the Supersonic Near Wake Flow Behind Blunt-Based Afterbodies-Reference-Cited by-同舟云学术

Effects of a Swirling Flow Motion on the Supersonic Near Wake Flow Behind Blunt-Based Afterbodies

Published:2017-06-02 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Fluid Dynamics Conference
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Author:

Weidner Stephan¹,Hruschka Robert¹,Rey Christian¹,Leopold Friedrich¹,Frohnapfel Bettina²,Seiler Friedrich²

Affiliation:

1. French-German Research Institute of Saint-Louis (ISL)

2. Karlsruhe Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3971

Reference24 articles.

1. Measurement of in-flight base pressure on an artillery-fired projectile

2. 2Leopold, F., Simulation und stabilitatstheoretische Untersuchungen zum kompressiblen Nachlauf eines langsangestromten Kreiszylinders, Ph.D. thesis, Technische Universität Braunschweig,1993, inGerman.

3. Supersonic base flow experiments in the near wake of a cylindrical afterbody

4. Effect of a rapid expansion on the development of compressible free shear layers

5. Navier-Stokes computations of projectile base flow with and without mass injection

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