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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
Results 15251 - 15260 of 16,845
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Investigation of ejection releases of an MB-1 rocket from a 0.04956-scaled model of the convair F-106A airplane at mach number 1.59

Investigation of ejection releases of an MB-1 rocket from a 0.04956-scaled model of the convair F-106A airplane at mach number 1.59

Date: May 20, 1957
Creator: Lee, J. B.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of curvature on the transition from laminar to turbulent boundary layer

The effect of curvature on the transition from laminar to turbulent boundary layer

Date: September 1, 1937
Creator: Clauser, M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Additional abstracts pertaining to seaplanes

Additional abstracts pertaining to seaplanes

Date: March 9, 1948
Creator: Bidwell, J. M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flutter experiments with various control configurations

Flutter experiments with various control configurations

Date: July 10, 1957
Creator: Boswinkle, R. W., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Turbine Engines for High-Speed Flight

Turbine Engines for High-Speed Flight

Date: January 1, 1958
Creator: Henneberry, H. M.
Description: This analysis investigates the application of gas turbine engines at a cruise Mach number of 4.
Contributing Partner: UNT Libraries Government Documents Department
Model ditching investigations of three airplanes equipped with hydro-skis

Model ditching investigations of three airplanes equipped with hydro-skis

Date: April 25, 1950
Creator: Fisher, L. J.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of nose shape and wing thickness ratio on the drag at zero lift of a missile having triangular wings and tails

Effect of nose shape and wing thickness ratio on the drag at zero lift of a missile having triangular wings and tails

Date: May 31, 1950
Creator: Hall, J. R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of suction-slot shapes for controlling a turbulent boundary layer

Investigation of suction-slot shapes for controlling a turbulent boundary layer

Date: June 1, 1947
Creator: Pierpont, P. K.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The resistance to air flow of porous materials suitable for boundary-layer-control applications using area suction

The resistance to air flow of porous materials suitable for boundary-layer-control applications using area suction

Date: January 1, 1954
Creator: Dannenberg, R. E.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of surface roughness and extreme cooling on boundary-layer transition for 15 deg cone-cylinder in free flight at Mach numbers to 7.6

Effects of surface roughness and extreme cooling on boundary-layer transition for 15 deg cone-cylinder in free flight at Mach numbers to 7.6

Date: March 5, 1958
Creator: Rabb, L.
Description: None
Contributing Partner: UNT Libraries Government Documents Department