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Control deflections, airplane response, and tail loads measured on an F-100A airplane in service operational flying
Report presenting the results from 20 hours of service operational flying of an instrumented North American F-100A fighter airplane. Results regarding the altitude and Mach number, normal-load factor, airplane attitude, use of controls, rolling motions, pitching motions, yawing motions, vertical-tail loads, horizontal-tail loads, and a comparison with other airplanes are provided.
Date:
June 5, 1958
Creator:
Pembo, Chris & Matranga, Gene J.
System:
The UNT Digital Library
Analysis of transonic rotor-blade passage loss with hot-wire anemometers
From Introduction: "This report presents data from measurements of the flow in a single-stage research compressor, which supports the model of reference 1. A calculated shock technique similar to that of reference 1 is incorporated with these experimental results. Another approach for estimating passage shock loss given a flow rate and blade geometry was reported in reference 2."
Date:
June 5, 1958
Creator:
Lewis, George W.; Tysl, Edward R. & Fessler, Theodore E.
System:
The UNT Digital Library