Pressure, recovery and mass-flow performance of four annular nose inlets operating in Mach number region of 3.1 and Reynolds number range of approximately 0.45 x 10(exp 6) to 2.20 x 10(exp 6)

Hunczak, Henry R
naca-rm-e54a07
March 26, 1954


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1954/naca-rm-e54a07.pdf