Mach 6 integrated systems testing for the Hypersonic Tunnel Facility-Reference-Cited by-同舟云学术

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Mach 6 integrated systems testing for the Hypersonic Tunnel Facility

Published:2000-06-19 Issue: Volume: Page:
ISSN:
Container-title:21st Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Woike Mark¹,Willis Brian¹

Affiliation:

1. NASA, Glenn Research Center, Sandusky, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-2446

Reference16 articles.

1. Mach 6 Integrated systems Tests of the NASA TM107083, December 1995. 5. Perkins, H.D.; Thomas, S.R.; and Pack, W.D.

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1. Multi-Objective Optimization Framework for Hypersonic Aerothermoelastic Scaling Laws and Its Application;AIAA Journal;2020-07

2. A Surrogate-Based Optimization Framework for Hypersonic Aerothermoelastic Scaling Laws with Application to Skin Panels;AIAA Scitech 2019 Forum;2019-01-06

3. Demonstration of Ethanol-Blended Hydrogen Peroxide Gas Generator for Ramjet Combustor Flow Simulation;Journal of Propulsion and Power;2018-05

4. Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel;Science China Technological Sciences;2015-01-30

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