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80-octane number air flow air-fuel ratio Aircraft Engine charge air charge-air and cooling-air CM CM COMMITTEE FOR AERONAUTICS constant cooling air cooling effectiveness cylinder barrel cylinder pressure decrease dimensional characteristics discharge drag coefficient duct engine power engine speed entrance-exit loss equation exhaust gas exhaust stack Fred Voss fron fuel fuel-air ratio given heat heat-transfer inches of mercury inches of water increase indicated mean effective inducted intercooler operating intercooler volume KN CM laminar flow Langley Field loss in engine maximum permissible mean effective pressure muff NACA nozzle area obtained operating conditions percent permissible indicated mean plate spacings plate thickness plate-type intercooler plotted pressure drop propeller propulsive efficiency quantity reference intercooler Reynolds number shown in figure specific fuel consumption steel surface-friction temperature thermal thermocouples thrust horsepower thrust power turbulent flow valve velocity-profile WARTIME REPORT water injection water-fuel ratio weight width