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Effect of Blade Loading of the Climb and High-Speed Performance of a Three-Blade Hamilton Standard No. 6507A-2 Propeller on a Republic P-47D Airplane
Report presenting climb and high-speed tests of a Hamilton Standard No. 6507A-2 three-blade propeller, which have been made to determine the effect of blade loading on propeller efficiency. The normal and military power climb efficiencies were found to be about equal at altitudes below 16,000 feet.
Date:
July 1945
Creator:
Gardner, John J.
System:
The UNT Digital Library
Determination of Induced Velocity in Front of an Inclined Propeller by a Magnetic-Analogy Method
Report presenting the horizontal and vertical components of the induced velocity in front of an inclined propeller in a horizontal stream obtained by a magnetic-analogy method. The problem was formulated in terms of the linear theory of the acceleration potential of an incompressible nonviscous fluid.
Date:
February 1946
Creator:
Gardner, Clifford S. & LaHatte, James A., Jr.
System:
The UNT Digital Library
Dynamic Loads on Airplane Structures During Landing
Report presenting the application of transient theory to the rational determination of dynamic loads on airplane structures during initial landing impact. Simplified procedures are described by which the distribution of the maximum attainable value of the dynamic stresses in the structure may be obtained.
Date:
October 1944
Creator:
Biot, M. A. & Bisplinghoff, R. L.
System:
The UNT Digital Library