Calculation of Strong Shock Wave Propagation in an Expansion Tube
Author:
Affiliation:
1. Tottori University
2. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Reference18 articles.
1. Basic characteristics of the free-piston driven expansion tube JAXA HEK-X
2. MacLean, M., Dufrene, A., Wadhams, T. and Holden, M. "Numerical and experimental characterization of high enthalpy flow in an expansion tunnel facility", AIAA Paper No. 20101562.
3. High-speed visualization for test-time evaluation of a JAXA HEK-X free-piston driven expansion tube
4. Numerical simulation of transient hypervelocity flow in an expansion tube
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1. CFD Simulation of HEK-X Expansion Tube Flowfield;AIAA SCITECH 2023 Forum;2023-01-19
2. Comparison of flight and shock tunnel spectroscopy of Hayabusa2 Sample Return Capsule;AIAA AVIATION 2022 Forum;2022-06-20
3. Aeroheating Measurement of HAYABUSA-CAPSULE using HEK-X Expansion Tube;AIAA Scitech 2021 Forum;2021-01-04
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