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[Dispersion of fission products]
This historic report is on letter which details the research into atmospheric dispersion of fissioviable materials in the event of a reactor accident at Savannah River Plant. Graphs are included.
Date:
October 29, 1956
Creator:
Menegus, R. L.
System:
The UNT Digital Library
THE CORROSION OF TYPE 304L STAINLESS STEEL BY SOLUTIONS OF NITRIC ACID- SODIUM DICHROMATE AND NITRIC-HYDROFLUORIC ACIDS
None
Date:
October 29, 1956
Creator:
Walker, W.L.
System:
The UNT Digital Library
H-10 coating waste: Redox
This report discusses the losses of uranium and plutonium in coating wastes.
Date:
October 29, 1956
Creator:
Shortess, C. J. & Johnson, W. H.
System:
The UNT Digital Library
Effect of several design variables on internal performance of convergent-plug exhaust nozzles
Numerous experiments were conducted to determine factors which affect the internal performance of convergent-plug exhaust nozzles. The results of these experiments, which include effects of such things as plug shape, nozzle inlet Mach number, and outer-shell characteristics, provide a basis for optimum desifn from the standpoint of weight and size. The results also show performance penalties which can result when the nozzle is too small.
Date:
October 29, 1956
Creator:
Krull, H. George; Beale, William T. & Schmiedlin, Ralph F.
System:
The UNT Digital Library
Experimental investigation of an overriding control to effect recovery from surge and stall in a turbojet engine
The override was designed to automatically recover the engine from stall and surge by reducing fuel flow and then increasing fuel flow in a manner to avoid repeated stalls and surges and successfully complete the acceleration. One of two parameters was used to operate the override, tailpipe temperature, or the derivative of compressor-discharge pressure. The override operating with tailpipe temperature recovered the engine from stall and surge. Operating on compressor-discharge-pressure derivative, the override recovered the engine from surge, but failed when stall was encountered.
Date:
October 29, 1956
Creator:
Stiglic, Paul M. & Heppler, Herbert
System:
The UNT Digital Library
Effect of fuselage circumferential inlet location on diffuser-discharge total-pressure profiles at supersonic speeds
An experimental investigation of the effect of angle of attack and inlet corrected air flow on diffuser-discharge total-pressure profiles of inlets located in various circumferential positions on a fuselage was conducted at supersonic speeds. Results indicated that the diffuser total-pressure profiles for a bottom inlet were least affected by angle of attack on distortion level was obtained with a side inlet. Variation in distortion for top inlets with angle of attack was confined to the supercritical range of inlet operation.
Date:
October 29, 1956
Creator:
Kremzier, Emil J. & Wasserbauer, Joseph F.
System:
The UNT Digital Library