Rapid Assessment on Flow Parameter Matching Scheme in Aerodynamic Testing in a Combustion Wind Tunnel
Author:
Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-319-44866-4_109
Reference10 articles.
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3. Andrews, E.H.: Scramjet development and testing in the United States. In: AIAA Paper 2001-1927
4. Edelman, R.B., Spadaccini, L.J.: Theoretical effects of vitiated air contamination on ground testing of hypersonic air breathing engines. J. Spacecr. 6(12), 1442–1447 (1969)
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