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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data

Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data

Date: June 17, 1954
Creator: Burrows, Dale L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow

The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow

Date: November 12, 1952
Creator: Love, Eugene S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An experimental study of five annular air inlet configurations at subsonic and transonic speeds

An experimental study of five annular air inlet configurations at subsonic and transonic speeds

Date: August 19, 1953
Creator: Pendley, Robert E; Bryan, Carroll R; Fleming, Frank F & Milillo, Joseph R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation to determine the horizontal- and vertical-tail contributions to the static lateral stability characteristics of a complete-model swept-wing configuration at high subsonic speeds

Wind-tunnel investigation to determine the horizontal- and vertical-tail contributions to the static lateral stability characteristics of a complete-model swept-wing configuration at high subsonic speeds

Date: July 10, 1953
Creator: Kuhn, Richard E; Fournier, Paul G & Wiggins, James W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Rocket-model investigation to determine the hinge-moment and normal-force properties of a full-span, constant-chord, partially balanced trailing-edge control on a 60 degree clipped delta wing between Mach numbers of 0.50 and 1.26

Rocket-model investigation to determine the hinge-moment and normal-force properties of a full-span, constant-chord, partially balanced trailing-edge control on a 60 degree clipped delta wing between Mach numbers of 0.50 and 1.26

Date: October 30, 1953
Creator: Martz, C William & Goslee, John W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A study of the use of various high-lift devices on the horizontal tail of a canard airplane model as a means of increasing the allowable center-of-gravity travel

A study of the use of various high-lift devices on the horizontal tail of a canard airplane model as a means of increasing the allowable center-of-gravity travel

Date: January 21, 1953
Creator: Johnson, Joseph L , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A polar-coordinate survey method for determining jet-engine combustion-chamber performance

A polar-coordinate survey method for determining jet-engine combustion-chamber performance

Date: September 1, 1955
Creator: Friedman, Robert & Carlson, Edward R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Study of screeching combustion in a 6-inch simulated afterburner

Study of screeching combustion in a 6-inch simulated afterburner

Date: October 1, 1955
Creator: Rayle, Warren D; Tower, Leonard K & Blackshear, Perry L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Measurements of the effect of trailing-edge thickness on the zero-lift drag of thin low-aspect-ratio wings

Measurements of the effect of trailing-edge thickness on the zero-lift drag of thin low-aspect-ratio wings

Date: November 1, 1955
Creator: Morrow, John D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A statistical study of wing lift at ground contact for four transport airplanes

A statistical study of wing lift at ground contact for four transport airplanes

Date: April 1, 1955
Creator: Lindquist, Dean C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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