Design of Vortex Generator Flow Control in Inlets
Author:
Affiliation:
1. Swedish Defence Research Agency FOI, 164 90 Stockholm, Sweden
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.21364
Reference35 articles.
1. Invited: Aerodynamic Flowfield Control Technologies for Highly Integrated Airframe Propulsion Flowpaths
2. Aircraft Engine Design, Second Edition
3. Design and Testing of a Blended Wing Body with Boundary Layer Ingestion Nacelles at High Reynolds Numbers (Invited)
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