A three-dimensional body-force model for nacelle-fan systems under inlet distortions
Author:
Funder
Boeing Company
Colorado State University
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference43 articles.
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2. Fan–intake interaction under high incidence;Cao;J. Eng. Gas Turbines Power,2016
3. Actuator duct model of turbomachinery components for powered-nacelle Navier-Stokes calculations;Hsiao;J. Propuls. Power,2001
4. Assessment methods for unsteady flow distortion in aero-engine intakes;Gil-Prieto;Aerosp. Sci. Technol.,2018
5. Characteristics of unsteady total pressure distortion for a complex aero-engine intake duct;Tanguy;Aerosp. Sci. Technol.,2018
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