Altitude performance of a 20-inch-diameter ram-jet engine investigated in a free-jet facility at Mach number 3.0

Altitude performance of a 20-inch-diameter ram-jet engine investigated in a free-jet facility at Mach number 3.0

Date: January 1, 1952
Creator: Smolak, G. R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Design of combustor for long-range ram-jet engine and performance of rectangular analog

Design of combustor for long-range ram-jet engine and performance of rectangular analog

Date: January 29, 1954
Creator: Koch, R. G.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Preliminary transient performance data on the fuel control of the XRJ47-W-5 ram-jet engine

Preliminary transient performance data on the fuel control of the XRJ47-W-5 ram-jet engine

Date: January 1, 1954
Creator: Smith, I. D.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Full-scale, free-jet investigation of methods of improving outlet flow distribution in a side-inlet supersonic diffuser

Full-scale, free-jet investigation of methods of improving outlet flow distribution in a side-inlet supersonic diffuser

Date: March 28, 1955
Creator: Farley, J. M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of three low-temperature-ratio combustor configurations in a 48-inch-diameter ram-jet engine

Investigation of three low-temperature-ratio combustor configurations in a 48-inch-diameter ram-jet engine

Date: March 10, 1954
Creator: Meyer, C. L.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Radiant heat transfer from flames in a single tubular turbojet combuctor

Radiant heat transfer from flames in a single tubular turbojet combuctor

Date: August 19, 1952
Creator: Topper, L.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A preliminary study of the effect of boric oxide deposits on the performance of two selected turbine stator-blade shapes

A preliminary study of the effect of boric oxide deposits on the performance of two selected turbine stator-blade shapes

Date: February 25, 1958
Creator: Nusbaum, W. J.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Interference effects of fuselage-stored missiles on inlet duct model of an interceptor-type aircraft at Mach numbers 1.5 to 1.9

Interference effects of fuselage-stored missiles on inlet duct model of an interceptor-type aircraft at Mach numbers 1.5 to 1.9

Date: April 24, 1957
Creator: Davis, O. H.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calculated performance of a direct-air nuclear turbojet-powered airplane using a split-flow reactor and a separated-type shield

Calculated performance of a direct-air nuclear turbojet-powered airplane using a split-flow reactor and a separated-type shield

Date: February 1, 1951
Creator: Doyle, R. B.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Experimental investigation of extreme internal flow turning at the cowl lip of an axisymetric inlet at a Mach number of 2.95

Experimental investigation of extreme internal flow turning at the cowl lip of an axisymetric inlet at a Mach number of 2.95

Date: May 13, 1958
Creator: Kowalski, K. L.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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