Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation

Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation

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<jats:title>Abstract</jats:title> <jats:p>This paper presents first-of-a-kind measurements, and complementary computations, of the flow through the propulsion system of a boundary layer ingesting, twin-engine advanced civil transport aircraft configuration. The expe...

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Bibliographic Details
Main Authors: Hall, DK, Greitzer, EM, Uranga, A, Drela, M, Pandya, SA
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Format: Article
Language:English
Published: ASME International 2022
Online Access:https://hdl.handle.net/1721.1/145336

Internet

https://hdl.handle.net/1721.1/145336

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