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EXTRUSION OF 2% U-Al ALLOY FUEL RODS FOR THE ARGONNE CP-3 REACTOR
None
Date:
July 26, 1950
Creator:
Manly, W.D.
System:
The UNT Digital Library
Investigation of Aerodynamic and Icing Characteristics of Water-Inertia-Separation Inlets for Turbojet Engines
"The results of an investigation of several internal water-inertia-separation inlets consisting of a main duct and an alternate duct designed to prevent automatically the entrance of large quantities of water into a turbojet engine in icing conditions are presented. Total-pressure losses and icing characteristics for a direct-ram inlet and the inertia-separation inlets are compared at similar aerodynamic and simulated icing conditions. Complete ice protection for inlet guide vanes could not be achieved with the inertia-separation inlets investigated" (p. 1).
Date:
July 26, 1950
Creator:
von Glahn, Uwe & Blatz, Robert E.
System:
The UNT Digital Library
The effects of compressibility on the pressures on a body of revolution and on the aerodynamic characteristics of a wing-nacelle combination consisting of the body of revolution mounted on a swept-back wing
Memorandum presenting an investigation of the effects of compressibility on the forces, pitching moments, and surface pressures on a wing-nacelle combination. The leading edge of the wing was swept back 37.25 degrees and the nacelle was a body of revolution with a fineness ratio of 6.5. The effects of compressibility on the surface pressures and on the drag of a body of revolution similar to the nacelle were also determined.
Date:
July 26, 1950
Creator:
Boltz, Frederick W. & Beam, Benjamin H.
System:
The UNT Digital Library
Advanced Seminar in Reactor Physics
The following report provides equations that result from a seminar in reactor physics.
Date:
July 26, 1950
Creator:
Smith, Nicholas M.
System:
The UNT Digital Library