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 Collection: National Advisory Committee for Aeronautics Collection
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
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
Analysis of pressure data obtained at transonic speeds on a thin low-aspect-ratio cambered delta wing-body combination

Analysis of pressure data obtained at transonic speeds on a thin low-aspect-ratio cambered delta wing-body combination

Date: September 26, 1958
Creator: Mugler, John P , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Heat Transfer Measured in Free Flight on a Slightly Blunted 25 deg Cone-Cylinder-Flare Configuration at Mach Numbers up to 9.89

Heat Transfer Measured in Free Flight on a Slightly Blunted 25 deg Cone-Cylinder-Flare Configuration at Mach Numbers up to 9.89

Date: September 26, 1958
Creator: Bond, Aleck C.; Lee, Dorothy B. & Rumsey, Charles B.
Description: Skin temperature and surface pressure of blunted cone-cylinder-flare configuration free flight test vehicle to hypersonic speeds.
Contributing Partner: UNT Libraries Government Documents Department
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
Effect of spike-tip and cowl-lip blunting on inlet performance of a Mach 3.0 external- compression inlet

Effect of spike-tip and cowl-lip blunting on inlet performance of a Mach 3.0 external- compression inlet

Date: September 23, 1958
Creator: Cubbison, R. N. & Samanich, N. E.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of spike-tip and cowl-lip blunting on inlet performance of a Mach 3.0 external-compression inlet

Effect of spike-tip and cowl-lip blunting on inlet performance of a Mach 3.0 external-compression inlet

Date: September 23, 1958
Creator: Cubbison, R W & Samanich, N E
Description: None
Contributing Partner: UNT Libraries Government Documents Department