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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
Results 15241 - 15250 of 18,582
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An experimental investigation of two internal-compression air-inlet designs which use fluid boundaries as a means of supersonic compression

An experimental investigation of two internal-compression air-inlet designs which use fluid boundaries as a means of supersonic compression

Date: August 14, 1958
Creator: Howell, Robert R & Trescot, Charles D , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Longitudinal and lateral aerodynamic characteristics at combined angles of attack and sideslip of a generalized missile model having a rectangular wing at a Mach number of 4.08

Longitudinal and lateral aerodynamic characteristics at combined angles of attack and sideslip of a generalized missile model having a rectangular wing at a Mach number of 4.08

Date: August 14, 1958
Creator: Smith, Fred M; Ulmann, Edwards F & Dunning, Robert W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of shock-trap bleed to improve pressure recovery of fixed-and variable-capture-area internal-contraction inlets; Mach number 2.0 to 3.0

Use of shock-trap bleed to improve pressure recovery of fixed-and variable-capture-area internal-contraction inlets; Mach number 2.0 to 3.0

Date: August 14, 1958
Creator: Luidens, Roger W & Flaherty, Richard J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of the effect of sweep and taper ratio on effectiveness of spoiler-slot-deflector controls on aspect-ratio-4 wings at transonic speeds

Wind-tunnel investigation of the effect of sweep and taper ratio on effectiveness of spoiler-slot-deflector controls on aspect-ratio-4 wings at transonic speeds

Date: August 14, 1958
Creator: Hammond, Alexander D & Mckinney, Linwood W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Maintenance of ETR Coolant

Maintenance of ETR Coolant

Date: August 15, 1958
Creator: Haas, F. C.
Description: Report describing the maintenance system in place for the coolant system of an Engineering Test Reactor (ETR).
Contributing Partner: UNT Libraries Government Documents Department
A Summary of Strontium 90 Analyses for Monthly Pot and Precipitation Collections

A Summary of Strontium 90 Analyses for Monthly Pot and Precipitation Collections

Date: August 18, 1958
Creator: U.S. Atomic Energy Commission. Health and Safety Laboratory.
Description: Report summarizing strontium 90 analyses collected throughout the world in order to determine the relationship between precipitation and nuclear fallout.
Contributing Partner: UNT Libraries Government Documents Department
Low-speed wind-tunnel tests of a 1/8-scale model of the bell d-188a vtol airplane

Low-speed wind-tunnel tests of a 1/8-scale model of the bell d-188a vtol airplane

Date: August 25, 1958
Creator: Mc Kinney, M. O. & Smith, C. C., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Experimental investigation of the effect of yaw on rates of heat transfer to transverse circular cylinders in a 6500-foot-per-second hypersonic air stream

Experimental investigation of the effect of yaw on rates of heat transfer to transverse circular cylinders in a 6500-foot-per-second hypersonic air stream

Date: August 26, 1958
Creator: Cunningham, Bernard E & Kraus, Samuel
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight investigation of a full-scale aircraft ejector with various spacing ratios and correlation with small-scale tests

Flight investigation of a full-scale aircraft ejector with various spacing ratios and correlation with small-scale tests

Date: August 26, 1958
Creator: Havill, C Dewey & Wingrove, Rodne C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Forces and pitching moments on an aspect-ratio-3.1 wing-body combination at Mach numbers from 2.5 to 3.5 and sublimation studies of the effect of single-elements roughness on the boundary-layer flow

Forces and pitching moments on an aspect-ratio-3.1 wing-body combination at Mach numbers from 2.5 to 3.5 and sublimation studies of the effect of single-elements roughness on the boundary-layer flow

Date: August 26, 1958
Creator: Hopkins, Edward J; Keating, Stephen J , Jr & Muhl, Richard R
Description: None
Contributing Partner: UNT Libraries Government Documents Department