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Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel
Gregory V. Selby1986
Género: Flow visualization
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Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
Emma Jean Landrum
1977
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Experimental Hydraulics : Methods, Instrumentation, Data Processing and Management : Volume II
Jochen Aberle
2017
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Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
Emma Jean Landrum
1979
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