Stanton tube calibration in a laminar boundary layer at Mach 6.
KUBOTA, T. /CALIFORNIA INST. OF TECH., GRADUATE AERONAUTICAL LABS., FIRESTONE FLIGHT SCIENCES LAB.,, LEWIS, J. E.
AIAA Journal ; 4 , 12 ; 2251-2252
1966
Article (Journal)
Electronic Resource
English
ROUGHNESS-INDUCED INSTABILITY IN A LAMINAR BOUNDARY LAYER AT MACH 6
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