Interference Effect of Engine Exhaust on Civil Aircraft Drag Performance
Author:
Affiliation:
1. Beijing University of Aeronautics and Astronautics, 100191 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031822
Reference5 articles.
1. Transonic Euler flow calculation around a transport configuration with powered engine effects
2. Benefits and costs of powered engine simulation at low speeds
3. Civil turbofan propulsion system integration studies using powered testing techniques at ARA, Bedford
4. Experimental techniques used to evaluate propulsion system interference effects on the cruise configuration of the Boeing C-14
5. Wind tunnel test techniques for powered lift airplanes
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2. Impact of installation on a civil large turbofan exhaust system at idle descent conditions;Aerospace Science and Technology;2021-12
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5. Drag prediction method of powered-on civil aircraft based on thrust drag bookkeeping;Chinese Journal of Aeronautics;2015-08
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