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SECTION 3 NOVEMBER 1941 NUMBER
Change in Airplane Performance Due to a Change
84 other sections not shown
Ae.E aerodynamic Aeronautical Review Aeronautical Sciences Aeroplane Air Corps air-cooled Aircraft Corp Aircraft Engineering airfoil airplane alloys altitude angle angle of attack application Aviation Award beam bomber buckling cent coefficient compression constant cooling Curtiss-Wright Corp curve cylinder density determined developed drag drag coefficient duct effect elastic equation equipment factor flange flight test fluid flying fuel gasoline given heat illus increase indicated industry Institute intercooler isentropic Journal machine material maximum ment method modulus N.A.C.A. Technical obtained October operation paper Paul Kollsman pilot plane Plastics plywood present pressure problem production propeller ratio Research Royal Aeronautical Society rubber September sheet shown in Fig speed stability stiffener stress stress-strain curves surface take-off throttle tion U.S. Army United United Aircraft Corp valve velocity weight wind tunnel wing loading Wright Brothers