The Effect of Diffuser Geometry on the Starting Pressure Ratio of a Supersonic Wind Tunnel
27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
01.01.2010
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
2010-4344 The Effect of Diffuser Geometry on the Starting Pressure Ratio of a Supersonic Wind Tunnel
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