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airplane aromatics auxiliary jet propulsion Barrel middle Barrel top benzene brake horsepower combustion-air temperature COMMITTEE FOR AERONAUTICS constant cooling air cooling-air pressure drop crankshaft curves determine engine speed equation ethylene dibromide exhaust-valve temperature fuel 11 ground run inches of mercury increase Indicated horsepower indicated mean effective inlet inlet-air temperature knock manifold pressure maximum blade-bearing load mean effective pressure mercury absolute mixture distribution NACA NATIONAL ADVISORY COMMITTEE nozzle obtained operating temperature orifice over-all fuel-air ratio performance piston plunger displacement propeller pump rate of discharge rate of plunger Rear spark-plug reduced ring s3iavaan shown in figure spark spark-plug bushing special baffles specific fuel consumption specific humidity standard baffles STANFORD UNIVERSITY strain gages stresses supercharger supercharger gear ratio take-off distance take-off velocity tappet tetraethyl lead thermocouple throttle setting thrust toluene values valve overlap variation vibrations WARTIME REPORT weight of fuel xylene