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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
Use of electric analog for calculation of temperature distribution of cooled turbine blades

Use of electric analog for calculation of temperature distribution of cooled turbine blades

Date: December 1, 1953
Creator: Ellerbrock, Herman H; Schum, Eugene F & Nachtigall, Alfred J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of fences to increase uniformity of boundary layer on side walls of supersonic wind tunnels

Use of fences to increase uniformity of boundary layer on side walls of supersonic wind tunnels

Date: July 16, 1952
Creator: Haefeli, Rudolph C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of flame-immersed blades to improve combustion limits and efficiency of a 5-inch diameter connected-pipe, ram-jet combustor

Use of flame-immersed blades to improve combustion limits and efficiency of a 5-inch diameter connected-pipe, ram-jet combustor

Date: April 9, 1953
Creator: Male, Donald 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
Use of main-inlet bypass to supply ejector exhaust nozzle at supersonic speeds

Use of main-inlet bypass to supply ejector exhaust nozzle at supersonic speeds

Date: February 28, 1957
Creator: Hearth, Donald P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The use of metallic inhibitors for eliminating mass transfer and corrosion in nickel and nickel alloys by molten sodium hydroxide

The use of metallic inhibitors for eliminating mass transfer and corrosion in nickel and nickel alloys by molten sodium hydroxide

Date: February 1, 1955
Creator: Forestieri, Americo F & Lad, Robert A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of nonlinearities to compensate for the effects of a rate-limited servo on the response of an automatically controlled aircraft

Use of nonlinearities to compensate for the effects of a rate-limited servo on the response of an automatically controlled aircraft

Date: January 1, 1955
Creator: Schmidt, Stanley F & Triplett, William C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The use of perforated inlets for efficient supersonic diffusion

The use of perforated inlets for efficient supersonic diffusion

Date: September 1, 1956
Creator: Evvard, John C & Blakey, John W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The use of pure twist for drag reduction on arrow wings with subsonic leading edges

The use of pure twist for drag reduction on arrow wings with subsonic leading edges

Date: August 1, 1957
Creator: Grant, Frederick C
Description: None
Contributing Partner: UNT Libraries Government Documents Department