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Investigation of the NACA 4-(5)(08)-03 Two-blade Propeller at Forward Mach Numbers to 0.925
West Point : A History of the United States Military Academy
Light Aircraft Engine Tests--Fuels And Operating Variables
Radiant heat transfer from flames in a single tubular turbojet combuctor
Investigation at Mach number 1.91 of spreading characteristics of jet expanding from choked nozzles
Index of NACA Technical Publications: June, 1951 - May, 1953