Trees on a Mountain Slope

Trees on a Mountain Slope

Access: Use of this item is restricted to the UNT Community.
Date: 1962
Creator: Thompson, Robert
Description: None
Contributing Partner: UNT College of Visual Arts + Design
Untitled (After Poussin)

Untitled (After Poussin)

Access: Use of this item is restricted to the UNT Community.
Date: 1964~
Creator: Thompson, Robert
Description: Painting of three red, yellow and blue figures. Two human figures and one blue animal figure in the middle of the composition. Green, red, light blue and peach landscape featuring trees, hills and gardens.
Contributing Partner: UNT College of Visual Arts + Design
Hinge-moment, lift, and pitching-moment characteristics of a flap-type control surface having various hinge-line locations on a 4-percent-thick 60 degree delta wing : transonic bump method

Hinge-moment, lift, and pitching-moment characteristics of a flap-type control surface having various hinge-line locations on a 4-percent-thick 60 degree delta wing : transonic bump method

Date: March 24, 1954
Creator: Thompson, Robert F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Simulated flight investigation of scaled-speed elastic swept-wing bomber and fighter models coupled wing tip to wing tip

Simulated flight investigation of scaled-speed elastic swept-wing bomber and fighter models coupled wing tip to wing tip

Date: February 14, 1956
Creator: Thompson, Robert F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of a 42.7 degree sweptback wing model to determine the effects of trailing-edge thickness on the aileron hinge-moment and flutter characteristics at transonic speeds

Investigation of a 42.7 degree sweptback wing model to determine the effects of trailing-edge thickness on the aileron hinge-moment and flutter characteristics at transonic speeds

Date: December 26, 1950
Creator: Thompson, Robert F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of horn balances on a 45 degree sweptback horizontal tail surface at high subsonic speeds

Investigation of horn balances on a 45 degree sweptback horizontal tail surface at high subsonic speeds

Date: December 3, 1948
Creator: Johnson, Harold S & Thompson, Robert F
Description: A wind-tunnel investigation of horn balances on a 45 degree sweptback, semispan, horizontal tail surface was made to determine the effects of horn size and inboard-edge fairing at a Mach number of 0.30 and to determine the effects of compressibility up to a Mach number of 0.89. Presented are lift, drag, pitching-moment, and hinge-moment data and lift and hinge-moment parameters.
Contributing Partner: UNT Libraries Government Documents Department
Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of a spoiler-slot-deflector control located at two spanwise positions

Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of a spoiler-slot-deflector control located at two spanwise positions

Date: November 19, 1954
Creator: Thompson, Robert F & Taylor, Robert T
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation at high subsonic speeds of a 45 sweptback Horizontal tail with plain and horn-balanced control surfaces

Investigation at high subsonic speeds of a 45 sweptback Horizontal tail with plain and horn-balanced control surfaces

Date: March 31, 1950
Creator: Johnson, Harold S & Thompson, Robert F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation by the transonic-bump method of a 35 degree sweptback semispan model equipped with a flap operated by a series of servovanes located ahead of and geared to the flap

Investigation by the transonic-bump method of a 35 degree sweptback semispan model equipped with a flap operated by a series of servovanes located ahead of and geared to the flap

Date: April 1, 1956
Creator: Phillips, William H & Thompson, Robert F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of control trailing-edge thickness or aspect ratio on the oscillating hinge-moment and flutter characteristics of a flap-type control at transonic speeds

Effect of control trailing-edge thickness or aspect ratio on the oscillating hinge-moment and flutter characteristics of a flap-type control at transonic speeds

Date: April 23, 1958
Creator: Moseley, William C , Jr & Thompson, Robert F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Hinge-moment and control-effectiveness characteristics of an outboard flap with an overhang nose balance on a tapered 35 degree sweptback wing of aspect ratio 4 : transonic-bump method

Hinge-moment and control-effectiveness characteristics of an outboard flap with an overhang nose balance on a tapered 35 degree sweptback wing of aspect ratio 4 : transonic-bump method

Date: August 28, 1952
Creator: Thompson, Robert F & Moseley, William C , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Oscillating hinge moments and flutter characteristics of a flap-type control surface on a 4-percent-thick unswept wing with low aspect ratio at transonic speeds

Oscillating hinge moments and flutter characteristics of a flap-type control surface on a 4-percent-thick unswept wing with low aspect ratio at transonic speeds

Date: February 23, 1956
Creator: Thompson, Robert F & Moseley, William C , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of hinge-line position on the oscillating hinge moments and flutter characteristics of a flap-type control at transonic speeds

Effect of hinge-line position on the oscillating hinge moments and flutter characteristics of a flap-type control at transonic speeds

Date: June 10, 1957
Creator: Thompson, Robert F & Moseley William C , JR
Description: None
Contributing Partner: UNT Libraries Government Documents Department
MARS Flight Engineering Status

MARS Flight Engineering Status

Date: April 6, 2010
Creator: Fast, James E.; Dorow, Kevin E.; Morris, Scott J.; Thompson, Robert C. & Willett, Jesse A.
Description: The Multi-sensor Airborne Radiation Survey Flight Engineering project (MARS FE) has designed a high purity germanium (HPGe) crystal array for conducting a wide range of field measurements. In addition to the HPGe detector system, a platform-specific shock and vibration isolation system and environmental housing have been designed to support demonstration activities in a maritime environment on an Unmanned Surface Vehicle (USV). This report describes the status of the equipment as of the end of FY09.
Contributing Partner: UNT Libraries Government Documents Department
Transportable Xenon Laboratory (TXL-1) Operations Manual

Transportable Xenon Laboratory (TXL-1) Operations Manual

Date: March 7, 2011
Creator: Thompson, Robert C.; Stewart, Timothy L.; Willett, Jesse A. & Woods, Vincent T.
Description: The Transportable Xenon Laboratory Operations Manual is a guide to set up and shut down TXL, a fully contained laboratory made up of instruments to identify and measure concentrations of the radioactive isotopes of xenon by taking air samples and analyzing them. The TXL is housed in a standard-sized shipping container. TXL can be shipped to and function in any country in the world.
Contributing Partner: UNT Libraries Government Documents Department