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Serial/Series Title: NACA Technical Notes

Collection: National Advisory Committee for Aeronautics Collection

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Thermal fatigue of ductile materials I : effect of variations in the temperature cycle on the thermal-fatigue of S-816 and inconel 550

Thermal fatigue of ductile materials I : effect of variations in the temperature cycle on the thermal-fatigue of S-816 and inconel 550

Thermal fatigue of ductile materials II : effect of cyclic thermal stressing on the stress-rupture life and ductility of S-816 and Inconel 550.

Thermal fatigue of ductile materials II : effect of cyclic thermal stressing on the stress-rupture life and ductility of S-816 and Inconel 550.

Torque-speed characteristics for high-specific-work turbines

Torque-speed characteristics for high-specific-work turbines

Transient temperature distribution in a two-component semi-infinite composite slab of arbitrary materials subjected to aerodynamic heating with a discontinuous change in equilibrium temperature or heat-transfer coefficient

Transient temperature distribution in a two-component semi-infinite composite slab of arbitrary materials subjected to aerodynamic heating with a discontinuous change in equilibrium temperature or heat-transfer coefficient

Use of short flat vanes for producing efficient wide-angle two-dimensional subsonic diffusers

Use of short flat vanes for producing efficient wide-angle two-dimensional subsonic diffusers

Use of the Coanda effect for jet deflection and vertical lift with multiple-flat-plate and curved-plate deflection surfaces

Use of the Coanda effect for jet deflection and vertical lift with multiple-flat-plate and curved-plate deflection surfaces

Use of the Kernel function in a three-dimensional flutter analysis with application to a flutter-tested delta-wing model

Use of the Kernel function in a three-dimensional flutter analysis with application to a flutter-tested delta-wing model

Water-impact theory for aircraft equipped with nontrimming hydro-skis mounted on shock struts

Water-impact theory for aircraft equipped with nontrimming hydro-skis mounted on shock struts

Wind-tunnel tests of a full-scale helicopter rotor with symmetrical and with cambered blade sections at advance ratios from 0.3 to 0.4

Wind-tunnel tests of a full-scale helicopter rotor with symmetrical and with cambered blade sections at advance ratios from 0.3 to 0.4

Boundary-layer Displacement Effects in Air at Mach Numbers of 6.8 and 9.6

Boundary-layer Displacement Effects in Air at Mach Numbers of 6.8 and 9.6

An approximate spin design criterion for monoplanes, 1 May 1939

An approximate spin design criterion for monoplanes, 1 May 1939

Methods of analyzing wind-tunnel data for dynamic flight conditions

Methods of analyzing wind-tunnel data for dynamic flight conditions

Spin tests of a low-wing monoplane to investigate scale effect in the model test range, May 1941

Spin tests of a low-wing monoplane to investigate scale effect in the model test range, May 1941

Remarks on the Pressure Distribution over the Surface of an Ellipsoid, Moving Translationally Through a Perfect Fluid

Remarks on the Pressure Distribution over the Surface of an Ellipsoid, Moving Translationally Through a Perfect Fluid

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