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  Partner: UNT Libraries Government Documents Department
 Resource Type: Report
 Decade: 1950-1959
The use of area suction for the purpose of delaying separation of air flow at the leading edge of a 63 degree swept-back wing : effects of controlling the chordwise distribution of suction air velocities

The use of area suction for the purpose of delaying separation of air flow at the leading edge of a 63 degree swept-back wing : effects of controlling the chordwise distribution of suction air velocities

Date: January 14, 1952
Creator: Cook, Woodrow L & Kelly, Mark W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The use of area suction for the purpose of improving trailing-edge flap effectiveness on a 35 degree sweptback wing

The use of area suction for the purpose of improving trailing-edge flap effectiveness on a 35 degree sweptback wing

Date: July 2, 1953
Creator: Holzhauser, Curt A; Cook, Woodrow L & Kelly, Mark W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The use of area suction to increase the effectiveness of a trailing-edge flap on a triangular wing of aspect ratio 2

The use of area suction to increase the effectiveness of a trailing-edge flap on a triangular wing of aspect ratio 2

Date: April 1, 1954
Creator: Kelly, Mark W & Tolhurst, William H , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of choked nozzle technique and exhaust jet diffuser for extending operable range of jet-engine research facilities

Use of choked nozzle technique and exhaust jet diffuser for extending operable range of jet-engine research facilities

Date: July 22, 1952
Creator: Povolny, John H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The use of cones as stabilizing and control surfaces at hypersonic speeds

The use of cones as stabilizing and control surfaces at hypersonic speeds

Date: August 12, 1957
Creator: Love, Eugene S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of constant diffuser Mach number as a control parameter for variable-geometry inlets at Mach numbers of 1.8 to 2.0

Use of constant diffuser Mach number as a control parameter for variable-geometry inlets at Mach numbers of 1.8 to 2.0

Date: November 4, 1957
Creator: Hearth, Donald P & Anderson, Bernhard H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of Constant Diffuser Mach Number as a Control Parameter for Variable-geometry Inlets at Mach Numbers of 1.8 to 2.0

Use of Constant Diffuser Mach Number as a Control Parameter for Variable-geometry Inlets at Mach Numbers of 1.8 to 2.0

Date: November 4, 1957
Creator: Anderson, B. H. & Hearth, D. P.
Description: Control of variable-geometry inlets at constant mach numbers with blunt lip diffuser.
Contributing Partner: UNT Libraries Government Documents Department
Use of effective momentum thickness in describing turbine rotor-blade losses

Use of effective momentum thickness in describing turbine rotor-blade losses

Date: May 14, 1956
Creator: Stewart, Warner L; Whitney, Warren J & Miser, James W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of electric analog for calculation of temperature distribution of cooled turbine blades

Use of electric analog for calculation of temperature distribution of cooled turbine blades

Date: December 1, 1953
Creator: Ellerbrock, Herman H; Schum, Eugene F & Nachtigall, Alfred J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of fences to increase uniformity of boundary layer on side walls of supersonic wind tunnels

Use of fences to increase uniformity of boundary layer on side walls of supersonic wind tunnels

Date: July 16, 1952
Creator: Haefeli, Rudolph C
Description: None
Contributing Partner: UNT Libraries Government Documents Department