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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
Results 15241 - 15250 of 18,906
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Experimental investigation of the drag due to wedges along the trailing edge of a swept wing

Experimental investigation of the drag due to wedges along the trailing edge of a swept wing

Date: June 27, 1958
Creator: Gambucci, Bruno J & Wyss, John A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
HRP Radiation Corrosion Studies: In-Pile Loop L-4-11

HRP Radiation Corrosion Studies: In-Pile Loop L-4-11

Date: June 27, 1958
Creator: McWherter, J. R.; Baker, J. E.; Bohlmann, E. G.; Bradley, N. C.; Jenks, G. H.; Jones, D. T. et al.
Description: Report issued by the Oak Ridge National Laboratory discussing radiation corrosion studies. As stated in the introduction, "the purpose of this experiment was to compare the performance of a large number of materials under similar irradiation and exposure conditions" (p. 1). This report includes tables, illustrations, and photographs.
Contributing Partner: UNT Libraries Government Documents Department
Hydrodynamic characteristics of missiles launched under water

Hydrodynamic characteristics of missiles launched under water

Date: June 27, 1958
Creator: Dawson, J. R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Maneuver performance of interceptor missiles

Maneuver performance of interceptor missiles

Date: June 27, 1958
Creator: Stone, D. G.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The prospects for laminar flow on hypersonic airplanes

The prospects for laminar flow on hypersonic airplanes

Date: June 27, 1958
Creator: Seiff, Alvin
Description: The factors which affect the extent of laminar flow on airplanes for hypersonic flight are discussed on the basis of the available data. Factors considered include flight Reynolds number, surface roughness, angle of attack, angle of leading-edge sweepback, and aerodynamic interference. Test data are presented for one complete configuration.
Contributing Partner: UNT Libraries Government Documents Department
A flight-test study of total-pressure distortion in a thick-lipped nose inlet

A flight-test study of total-pressure distortion in a thick-lipped nose inlet

Date: June 30, 1958
Creator: Wingrove, Rodney C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of the static stability characteristics of five hypersonic missile configurations at Mach numbers from 2.29 to 4.65

Investigation of the static stability characteristics of five hypersonic missile configurations at Mach numbers from 2.29 to 4.65

Date: June 30, 1958
Creator: Turner, Kenneth L & Appich, W H , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of the static stability characteristics of five hypersonic missile configurations at Mach numbers from 2.29 to 4.65

Investigation of the static stability characteristics of five hypersonic missile configurations at Mach numbers from 2.29 to 4.65

Date: June 30, 1958
Creator: Appich, W. H., Jr. & Turner, K. L.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic investigation of yawed wings of aspect ratios 3 and 6 with a Sears-Haack body and with symmetrical and asymmetrical bodies indented for a Mach number of 1.20

Transonic investigation of yawed wings of aspect ratios 3 and 6 with a Sears-Haack body and with symmetrical and asymmetrical bodies indented for a Mach number of 1.20

Date: June 30, 1958
Creator: Holdaway, George H & Hatfield, Elaine W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Viscous flows in inlets

Viscous flows in inlets

Date: June 30, 1958
Creator: Scherrer, Richard; Lundell, John H & Anderson, Lewis A
Description: None
Contributing Partner: UNT Libraries Government Documents Department