A wind tunnel investigation of panel response to boundary layer pressure fluctuations at Mach 1.4 and Mach 3.5
1966
III, 81 S
Ill., graph. Darst
Contract no.: NASw-932
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
A MACH 4 WIND TUNNEL FOR PLASMA / BOUNDARY LAYER INTERACTION STUDIES
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