A pressure-distribution investigation of a supersonic aircraft fuselage and calibration of the Mach number 1.59 nozzle of the Langley 4- by 4- foot supersonic tunnel

Cooper, Morton Smith, Norman F Kainer, Julian H
naca-rm-l9e27a
July 29, 1949

No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1949/naca-rm-l9e27a.pdf