Computational Assessment of the Boundary Layer Ingesting Nacelle Design of the D8 Aircraft
Author:
Affiliation:
1. NASA Ames Research Center
2. Massachusetts Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0907
Reference23 articles.
1. The Jet Airplane Utilizing Boundary Layer Air for Propulsion
2. 5Lynch, F. “A theoretical Investigation of the Effect of Ingesting Boundary Layer Air on Turbofan Engine Fuel Consumption,” Douglas Aircraft Report SM23981, May 1960.
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