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A correlation of loadings and afterbody length-beam ratios of various flying-boat hulls
"The gross weight, beam, and afterbody length of 12 contemporary flying boats and amphibians with pointed afterbodies are tabulated and correlated. For most of the hulls considered, the afterbody length-beam ratios are shown to be directly proportion to the gross-load coefficients" (p. 1).
Date:
June 1946
Creator:
Parkinson, John B.
System:
The UNT Digital Library
Progress Report on Strength and Creep of Special Ceramic Bodies in Tension at Elevated Temperatures
Report presenting an investigation for the determination of the behavior of ceramic bodies in tension at elevated temperatures for the purpose of determining data for the design of ceramic blades for gas turbines. Observations were made of six special ceramic bodies in order to determine their tensile strength and creep during prolonged loading under a range of stresses and temperatures.
Date:
June 1946
Creator:
Geller, R. F. & Burdick, M. D.
System:
The UNT Digital Library
A Correlation of the Effects of Compression Ratio and Inlet-Air Temperature on the Knock Limits of Aviation Fuels in a CFR Engine 2
Report presenting the knock-limited performance of nine fuels comprising isolated members of four classes of hydrocarbons in the form of three-dimensional plots of fuel-air ratio, compression temperature, and compression-air density.
Date:
June 1946
Creator:
Alquist, Henry E.; O'Dell, Leon & Evvard, John C.
System:
The UNT Digital Library