NASA NTRS · 19950012733
Impact of dynamic loads on propulsion integration
Abstract
Aircraft dynamic loads produced by engine exhaust plumes are examined for a class of military fighter and bomber configurations in model and full scale. The configurations examined are associated with the USAF F-15 and B-1B aircraft, and the US F-18 HARV and ASTOVL programs. The experience gained as a result of these studies is used to formulate a level of understanding concerning this phenomena that could be useful at the preliminary stage of propulsion/airframe design.
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Seiner, J. M.. 1994-09-01. Impact of dynamic loads on propulsion integration. https://ntrs.nasa.gov/citations/19950012733
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