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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
Results 15291 - 15300 of 17,329
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Large-scale wind-tunnel tests of a jet-transport-type model with leading- and trailing-edge high-lift devices

Large-scale wind-tunnel tests of a jet-transport-type model with leading- and trailing-edge high-lift devices

Date: September 26, 1958
Creator: Aoyagi, Kiyoshi & Hickey, David H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Static and dynamic-rotary stability derivatives of an airplane model with an unswept wing and a high horizontal tail at Mach numbers of 2.5, 3.0, and 3.5

Static and dynamic-rotary stability derivatives of an airplane model with an unswept wing and a high horizontal tail at Mach numbers of 2.5, 3.0, and 3.5

Date: September 26, 1958
Creator: Lampkin, Bedford A & Tunnell, Phillips J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some notes on the probable damage to an intercontinental-ballistic-missile warhead following puncture of the heat shield

Some notes on the probable damage to an intercontinental-ballistic-missile warhead following puncture of the heat shield

Date: September 28, 1958
Creator: Strass, H. K. & Goodman, V. M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Combustor performance with various hydrogen-oxygen injection methods in a 200-pound-thrust rocket engine

Combustor performance with various hydrogen-oxygen injection methods in a 200-pound-thrust rocket engine

Date: September 30, 1958
Creator: Heidmann, M F & Baker, Louis, Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Off-Design Performance of Divergent Ejectors

Off-Design Performance of Divergent Ejectors

Date: September 30, 1958
Creator: Beheim, M. A.
Description: Off-design performance of divergent ejectors.
Contributing Partner: UNT Libraries Government Documents Department
Off-design performance of divergent ejectors

Off-design performance of divergent ejectors

Date: September 30, 1958
Creator: Beheim, Milton A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Rocket-model investigation to determine the lift and pitching effectiveness of small pulse rockets exhausted from the fuselage over the surface of an adjacent wing at Mach numbers from 0.9 to 1.8

Rocket-model investigation to determine the lift and pitching effectiveness of small pulse rockets exhausted from the fuselage over the surface of an adjacent wing at Mach numbers from 0.9 to 1.8

Date: September 30, 1958
Creator: Martz, C William
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Screaming tendency of the gaseous-hydrogen - liquid-oxygen propellant combination

Screaming tendency of the gaseous-hydrogen - liquid-oxygen propellant combination

Date: September 30, 1958
Creator: Baker, Louis, Jr & Steffen, Fred W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of highly reactive chemical additives to improve afterburner performance at altitude

Use of highly reactive chemical additives to improve afterburner performance at altitude

Date: September 30, 1958
Creator: Sivo, J. N. & Wanhainen, J. P.
Description: Liquid hydrogen and aluminum trimethyl as highly reactive chemical additives in turbojet afterburner to promote fuel combustion process.
Contributing Partner: UNT Libraries Government Documents Department
Use of highly reactive chemical additives to improve afterburner performance at altitude

Use of highly reactive chemical additives to improve afterburner performance at altitude

Date: September 30, 1958
Creator: Wanhainen, John P & Sivo, Joseph N
Description: None
Contributing Partner: UNT Libraries Government Documents Department