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NACA Research Memorandums
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/
Experimental investigation of laminar-boundary-layer control on an airfoil section equipped with suction slots located at discontinuities in the surface pressure distribution
Date: December 15, 1953
Creator: Horton, E. A.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc53185/
Experimental investigation of effects of simulated nacelles and wing-root freedoms on supersonic flutter characteristics of a cambered, modified, swept, tapered wing
Date: October 16, 1957
Creator: Hanson, P. W.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc53182/
Experimental investigation of the stability, control, and induced rolling moments of a canard missile airframe at a Mach number of 1.7
Date: September 23, 1952
Creator: Chubb, R. S.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc53181/
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/