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aileron airplane angle of attack approximately assumed axis belly band blade element buoyancy calculated center of pressure combustion COMMITTEE FOR AERONAUTICS compression pressure compression ratio constant cords curve cylinder wall decrease deflection density determined detonation diameter displacement drag coefficient drain holes dynamical pressure edge efficiency elevator energy losses engine equation explosion pressures fabric filled with air formula friction fuel full-size airship give Goodyear Rubber Company hence horsepower inches increase Internal Combustion Engines lift coefficient lift/drag load maximum mi/hr Munk NATIONAL ADVISORY COMMITTEE neutral NOTES ON PROPELLER number of blades obtained oil film oil pressure piston rings preignition produced propeller blades ring groove rudder scraper rings seaplane slip stream loss spark advance speed stroke surface sylphon tan6 TECHNICAL NOTE temperature tests throttle thrust tion top center variable velocity of flight weight