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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Collection: National Advisory Committee for Aeronautics Collection
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
On the design of airfoils in which the transition of the boundary layer is delayed

On the design of airfoils in which the transition of the boundary layer is delayed

Date: October 1, 1952
Creator: Tani, I.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Study of chromium-frit-type coatings for high-temperature protection of molybdenum

Study of chromium-frit-type coatings for high-temperature protection of molybdenum

Date: July 1, 1951
Creator: Moore, D G
Description: The achievement of more compact and efficient power plants for aircraft is dependent, among other factors, on the perfection of heat-resisting materials that are superior to those in current use. Molybdenum is one of the high-melting metals (melting point, 4750 F). It is fairly abundant and also can be worked into many of the shapes required in modern power plants. To permit its widespread use at elevated temperatures, however, some means must first be found to prevent its rapid oxidation. The application of a protective coating is one method that might be used to achieve this goal. In the present work, a number of chromium-frit-type coatings were studied. These were bonded to molybdenum specimens by firing in controlled atmospheres to temperatures in the range of 2400 to 2700 F.
Contributing Partner: UNT Libraries Government Documents Department
Experimental investigation of laminar-boundary-layer control on an airfoil section equipped with suction slots located at discontinuities in the surface pressure distribution

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
Experimental investigation of effects of simulated nacelles and wing-root freedoms on supersonic flutter characteristics of a cambered, modified, swept, tapered wing

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
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