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aerodynamic aeronautical ailerons aircraft airflow airfoil airplane altitude Ames Laboratory angle blades bomber cent Cleveland combustion compressibility compressor cooling cowling cylinder device dive drag duct effect efficiency equipment experimental experiments feet fighter flaps flight research flight tests flow flying forces fuel full-scale tunnel fuselage gases gasoline heat high speed high-speed higher horizontal tail horsepower hull improved inch increase inlet installed instruments investigation jet propulsion Langley Field Langley Laboratory leading edge lift coefficient loads Mach number measurements ment miles per hour models moving NACA nose operation performance pilot piston plane pounds pressure problem propeller Propulsion Research ram-jet ratio revolutions per minute rivet rocket rotating rudder seaplane shape shock waves speed of sound stability and control stiffeners stresses structure studies supercharger supersonic surface take-off temperature test section thrust tion transonic triptane turbine turbo-jet engine turbulence velocity weight wind tunnel