Quasi-one-dimensional modeling of a free-piston shock tunnel
Author:
Affiliation:
1. University of Queensland, St. Lucia, Queensland 4072, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11961
Reference28 articles.
1. Hypervelocity real gas capabilities of GASL's expansion tube (HYPULSE) facility
2. Role and techniques of ground testing for simulation of flows up to orbital speed
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