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acceleration air-fuel ratio aircraft airplane Albatros L 83 amplitude angle autogiro axis bending blade boundary layer buckling combustion Committee for Aeronautics compression computed constant consumption crankshaft curvature jump curve cylinder deflection diameter drag coefficient duralumin effect elevator engine equation factor fatigue strength flight flow frequency friction fuel function gas cylinder gust holes horsepower ignition increase injection period injection pressure injector limit load cycles load reversals maximum measurements millimeters NACA Technical Memorandum needle normal force nozzles number of load obtained operation oscillation peak pressure percent piston pitot tube plastics plate polygons pump chamber ratio reference result Reynolds number rotor serrated shearing stress specific specific fuel consumption speed STANFORD UNIVERSITY STANFORD UNIVERSITY LIBRARIES static strain stress surface temperature tension lugs tion torsional transverse tubing twist values velocity wall wing structure Winterthur