Crossflow Fan Power Requirements for Boundary-Layer Suction in Transonic Flow
Author:
Affiliation:
1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801
Funder
NASA LEARN Grant
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034193
Reference15 articles.
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2. Sensitivity of Mission Energy Consumption to Turboelectric Distributed Propulsion Design Assumptions on the N3-X Hybrid Wing Body Aircraft
3. Preliminary Experimental Assessment of the Boundary Layer Ingestion Benefit for the D8 Aircraft
4. BradleyM.DroneyC. “Subsonic Ultra Green Aircraft Research: Phase I Final Report,” NASA CR2011-216847, April 2011.
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