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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1951
 Serial/Series Title: NACA Technical Notes
 Collection: National Advisory Committee for Aeronautics Collection
The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow

The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow

Date: October 1, 1951
Creator: Chang, Chieh-Chien
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow

Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow

Date: September 1, 1951
Creator: Watkins, Charles E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of an x-ray absorption method for measurement of high gas temperatures

An analysis of an x-ray absorption method for measurement of high gas temperatures

Date: December 1, 1951
Creator: Weltmann, Ruth N
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of flow in rotating passage of large radial-inlet centrifugal compressor at tip speed of 700 feet per second

An analysis of flow in rotating passage of large radial-inlet centrifugal compressor at tip speed of 700 feet per second

Date: December 1, 1951
Creator: Prian, Vasily D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of pure-bending flutter of a cantilever swept wing and its relation to bending-torsion flutter

Analysis of pure-bending flutter of a cantilever swept wing and its relation to bending-torsion flutter

Date: September 1, 1951
Creator: Cunningham, H J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analytic determination of the flow behind a symmetrical curved shock

An analytic determination of the flow behind a symmetrical curved shock

Date: October 1, 1951
Creator: Lin, C C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An Analytical and Experimental Investigation of the Skin Friction of the Turbulent Boundary Layer on a Flat Plate at Supersonic Speeds

An Analytical and Experimental Investigation of the Skin Friction of the Turbulent Boundary Layer on a Flat Plate at Supersonic Speeds

Date: February 1, 1951
Creator: Rubesin, Morris W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical evaluation of aerodynamic characteristics of turbines with nontwisted rotor blades

Analytical evaluation of aerodynamic characteristics of turbines with nontwisted rotor blades

Date: May 1, 1951
Creator: Slivka, William R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analytical investigation of effect of high-lift flaps on take-off of light airplanes

An analytical investigation of effect of high-lift flaps on take-off of light airplanes

Date: September 1, 1951
Creator: Weick, Fred E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical investigation of fully developed laminar flow in tubes with heat transfer with fluid properties variable along the radius

Analytical investigation of fully developed laminar flow in tubes with heat transfer with fluid properties variable along the radius

Date: July 1, 1951
Creator: Deissler, Robert G
Description: Relations were analytically obtained for the prediction of radial distributions of velocity and temperature for fully developed laminar flow of gases and of liquid metals in tubes with fluid properties variable along the radius. The relations are applicable to both heating and cooling of the fluid. By use of the relations for velocity and temperature distributions, relations were obtained among Nusselt number, friction parameter, and ratio of wall to bulk temperature. The Nusselt number and friction parameter were found to be independent of Reynolds number and Prandtl number. The effects of ratio of wall to bulk temperature on Nusselt number and friction parameter could be eliminated by evaluating the fluid properties at specified temperatures in the fluid.
Contributing Partner: UNT Libraries Government Documents Department
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