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 Collection: Technical Report Archive and Image Library
Results 15391 - 15400 of 18,906
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A cooled-gas pyrometer for use in high-temperature gas streams

A cooled-gas pyrometer for use in high-temperature gas streams

Date: September 1, 1958
Creator: Krause, Lloyd N; Johnson, Robert C & Glawe, George E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Cumulative fatigue damage at elevated temperature

Cumulative fatigue damage at elevated temperature

Date: September 1, 1958
Creator: Rey, William K
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Degassing Sparger Plate Screening Tests

Degassing Sparger Plate Screening Tests

Date: September 1958
Creator: Starkweather, D. C.
Description: Results of tests to remove fission gases, xenon and krypton, formed during the operation of a nuclear reactor.
Contributing Partner: UNT Libraries Government Documents Department
Effect of advance ratio on flight performance of a modified supersonic propeller

Effect of advance ratio on flight performance of a modified supersonic propeller

Date: September 1, 1958
Creator: Hammack, Jerome B & O'Bryan, Thomas C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of free-stream turbulence on heat transfer from a flat plate

The effect of free-stream turbulence on heat transfer from a flat plate

Date: September 1, 1958
Creator: Sugawara, Sugao; Sato, Takashi; Komatsu, Hiroyasu & Osaka, Hiroichi
Description: Turbulence was generated by using screens, and the turbulence percentage was measured by a hot-wire anemometer both in the boundary layer and the free stream. The local heat-transfer coefficient was measured at 12 locations along the plate for the cases of various turbulence levels. The transition Reynolds number from laminar to turbulent flow decreases as the main-stream turbulence level increases. In the range of laminar heat transfer the effect of turbulence in the main flow was not great, but in the range of turbulent heat transfer the heat-transfer coefficient increases according to the increase of turbulence.
Contributing Partner: UNT Libraries Government Documents Department
Effect of precipitate particles on creep of aluminum-copper alloys during age hardening

Effect of precipitate particles on creep of aluminum-copper alloys during age hardening

Date: September 1, 1958
Creator: Underwood, E E; Marsh, L L & Manning, G K
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of pressure and duct geometry on bluff-body flame stabilization

Effect of pressure and duct geometry on bluff-body flame stabilization

Date: September 1, 1958
Creator: Potter, Andrew E , Jr & Wong, Edgar L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of some external crosswise stiffeners on the heat transfer and pressure distribution on a flat plate at Mach numbers of 0.77, 1.39, and 1.98

Effect of some external crosswise stiffeners on the heat transfer and pressure distribution on a flat plate at Mach numbers of 0.77, 1.39, and 1.98

Date: September 1, 1958
Creator: Carter, Howard S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of compressibility on rotor hovering performance and synthesized blade-section characteristics derived from measured rotor performance of blades having NACA 0015 airfoil tip sections

Effects of compressibility on rotor hovering performance and synthesized blade-section characteristics derived from measured rotor performance of blades having NACA 0015 airfoil tip sections

Date: September 1, 1958
Creator: Shivers, James P & Carpenter, Paul J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of frequency and amplitude on the yawing derivatives of triangular, swept, and unswept wings and of a triangular-wing-fuselage combination with and without a triangular tail performing sinusoidal yawing oscillations

Effects of frequency and amplitude on the yawing derivatives of triangular, swept, and unswept wings and of a triangular-wing-fuselage combination with and without a triangular tail performing sinusoidal yawing oscillations

Date: September 1, 1958
Creator: Letko, William & Fletcher, Herman S
Description: None
Contributing Partner: UNT Libraries Government Documents Department