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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
Results 15251 - 15260 of 17,329
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A theoretical study of stagnation-point ablation.

A theoretical study of stagnation-point ablation.

Date: September 1, 1958
Creator: Roberts, Leonard
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The theory of diffusion in strained systems

The theory of diffusion in strained systems

Date: September 1, 1958
Creator: Girifalco, Louis A & Grimes, Hubert H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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

Date: September 1, 1958
Creator: Clauss, Francis J & Freeman, James W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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.

Date: September 1, 1958
Creator: Clauss, Francis J & Freeman, James W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Torque-speed characteristics for high-specific-work turbines

Torque-speed characteristics for high-specific-work turbines

Date: September 1, 1958
Creator: Stewart, Warner L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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

Date: September 1, 1958
Creator: Trimpi, Robert L & Jones, Robert A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The Turbulent Boundary Layer on a Rough Curvilinear Surface

The Turbulent Boundary Layer on a Rough Curvilinear Surface

Date: September 1, 1958
Creator: Droblenkov, V. F.
Description: A number of semiempirical approximate methods exist for determining the characteristics of the turbulent boundary layer on a curvilinear surface. At present, among these methods, the one proposed by L. G. Loitsianskii is given frequent practical application. This method is sufficiently effective and permits, in the case of wing profiles with technically smooth surfaces, calculating the basic characteristics of the boundary layer and the values of the overall drag with an accuracy which suffices for practical purposes. The idea of making use of the basic integral momentum equation ((d delta(sup xx))/dx) + ((V' delta(sup xx))/V) (2 + H) = (tau(sub 0))/(rho V(exp 2)) proves to be fruitful also for the solution of the problems in the determination of the characteristics of the turbulent boundary layer on a rough surface.
Contributing Partner: UNT Libraries Government Documents Department
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

Date: September 1, 1958
Creator: Cochran, D L & Kline, S J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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

Date: September 1, 1958
Creator: Von Glahn, Uwe H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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

Date: September 1, 1958
Creator: Woolston, Donald S & Sewall, John L
Description: None
Contributing Partner: UNT Libraries Government Documents Department