Technical notes / National Advisory Committee for Aeronautics

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Späterer Titel:USA. National Aeronautics and Space Administration Technical note / D
Körperschaft: USA National Advisory Committee for Aeronautics (VerfasserIn)
Format: UnknownFormat
Veröffentlicht: Washington, DC 1920-1958
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Titel Jahr Band
Some effects of vanes and of turbulence in two-dimensional wide-angle subsonic diffusers 1958
Low tire friction and cornering forces on a wet surface 1958
Drop-size distribution for crosscurrent breakup of liquid jets in airstream 1958
Practical solution of plastic deformation problems in elastic-plastic range 1958
Vibration survey of four representative types of air-cooled turbine blades 1958
Mechanical properties of pneumatic tires with special reference to modern aircraft tires 1958
Theoretical calculations of supersonic wave drag at zero lift for a particular store arrangement 1958
Stall propagation in a cascade of airfoils 1958
Theoretical investigation of subsonic oscillatory blade-row aerodynamics 1958
Fatigue behavior of aircraft structural beams 1958
Wall pressure fluctuations in a turbulent boundary layer 1958
Approximations for the thermodynamic and transport properties of high-temperature air 1958
Experimental investigation of turbojet-engine multiple-loop controls for nonafterburning and afterburning modes of engine operation 1958
Effect of cyclic thermal stressing on the stress-rupture life and ductility of S-816 and Inconel 550 1958
Noise survey under static conditions of a turbine-driven full-scale modified supersonic propeller ratio of 3.2 advance ratio of 3.2 1958
Investigation of spoilers at a Mach number of 1.93 to determine the effects of height and chordwise location on the section aerodynamic characteristics of a two-dimensional wing 1958
High-speed hydrodynamic characteristics of a flat plate and 20° dead-rise surface in unsymmetrical planing conditions 1958
Charts relating the compressice and shear buckling stresses of longitudinally supported plates to the effective deflectional stiffness of the supports 1958
Lift and moment on thin arrowhead wings with supersonic edges oscillating in symmetrical flapping and roll and application to the flutter of an all-movable control surface 1958
Effects of airplane flexibility on wing strains in rough air at 35,000 feet as determined by a flight investigation of a large swept-wing airplane 1958
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