You limited your search to:

  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Advanced Restricted Report
 Collection: Technical Report Archive and Image Library
Column and plate compressive strengths of aircraft structural materials : extruded 75S-T aluminum alloy

Column and plate compressive strengths of aircraft structural materials : extruded 75S-T aluminum alloy

Date: July 1, 1945
Creator: Roy, J Albert
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Column and plate compressive strengths of aircraft structural materials : extruded R303-T aluminum alloy

Column and plate compressive strengths of aircraft structural materials : extruded R303-T aluminum alloy

Date: October 1, 1945
Creator: Fay, Douglas P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparative cooling of cylinders of nonuniform fin width with tight-fitting baffles and with baffles that provide constant flow-path areas

Comparative cooling of cylinders of nonuniform fin width with tight-fitting baffles and with baffles that provide constant flow-path areas

Date: April 1, 1944
Creator: Buckner, Howard A , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A comparative study of the effect of wing flutter shape on the critical flutter speed

A comparative study of the effect of wing flutter shape on the critical flutter speed

Date: November 1, 1943
Creator: Pinkel, I Irving
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparison between calculated and measured loads on wing and horizontal tail in pull-up maneuvers

Comparison between calculated and measured loads on wing and horizontal tail in pull-up maneuvers

Date: October 1, 1945
Creator: Matheny, Cloyce E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparison of an approximate and an exact method of shear-lag analysis

Comparison of an approximate and an exact method of shear-lag analysis

Date: January 1, 1944
Creator: Duberg, John E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A comparison of analytically and experimentally determined isothermal pressure losses in a heat-exchanger installation

A comparison of analytically and experimentally determined isothermal pressure losses in a heat-exchanger installation

Date: May 1, 1945
Creator: Hillendahl, Wesley H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in the Langley 20-foot free-spinning tunnel

Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in the Langley 20-foot free-spinning tunnel

Date: March 1, 1946
Creator: Malvestuto, Frank S , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A comparison of the effects of four-blade dual- and single-rotation propellers on the stability and control characteristics of a high-powered single-engine airplane

A comparison of the effects of four-blade dual- and single-rotation propellers on the stability and control characteristics of a high-powered single-engine airplane

Date: June 1, 1944
Creator: Wick, Bradford M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A comparison of two flight-test procedures for the determination of aileron control capabilities of an airplane

A comparison of two flight-test procedures for the determination of aileron control capabilities of an airplane

Date: July 1, 1945
Creator: Skoog, Richard B
Description: None
Contributing Partner: UNT Libraries Government Documents Department