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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
Experimental Investigation of the Effect of Rear-fuselage Shape on Ditching Behavior
LIGHT AIRCRAFT TURBO-PROPELLER INSTALLATIONS
Effect of airplane configuration on static stability at subsonic and transonic speeds
Factors affecting the flow distortions produced by supersonic inlets
Minimum wave drag for arbitrary arrangements of wings and bodies
Flow field effects on static stability and control at high supersonic Mach numbers