Experimental Study of Boundary-Layer Ingestion into a Diverterless S-Duct Intake
Author:
Affiliation:
1. Institute of Aerodynamics and Flow Technology, DLR, German Aerospace Center, D-37073 Göttingen, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053902
Reference15 articles.
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3. Power Balance in Aerodynamic Flows
4. ArntzA.AtinaultO.DestaracD.MerlenA. “Exergy-Based Aircraft Aeropropulsive Performance Assessment: CFD Application to Boundary Layer Ingestion,” AIAA Paper 2014-2573, 2014.
5. Experimental and Computational Evaluation of Flush-Mounted, S-Duct Inlets
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