Shock Tube as a Device for Testing Transonic Airfoils at High Reynolds Numbers
Year: 1979
Type: article
Source: AIAA Journal
DOI: 10.2514/3.61208
Institutions: Iowa State University, Ames Research Center
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W2073178797
