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
Permallink:digital.library.unt.edu/ark:/67531/metadc53178/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc53174/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc53179/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc53176/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc53173/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc53295/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc53187/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc53188/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc53184/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc53189/