NASA NTRS · 19880028000
In-flight thrust determination
Abstract
The major aspects of processes that may be used for the determination of in-flight thrust are reviewed. Basic definitions are presented as well as analytical and ground-test methods for gathering data and calculating the thrust of the propulsion system during the flight development program of the aircraft. Test analysis examples include a single-exhaust turbofan, an intermediate-cowl turbofan, and a mixed-flow afterburning turbofan.
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Abernethy, Robert B., Adams, Gary R., Ascough, John C., Baer-Riedhart, Jennifer L., Balkcom, George H., Biesiadny, Thomas. 1986-01-01. In-flight thrust determination. https://ntrs.nasa.gov/citations/19880028000
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