Aerodynamic effects of lift-jet and lift-fan inlets in transition flight.
Author:
Affiliation:
1. Northrop Corporation, Norair Division, Hawthorne, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44022
Reference11 articles.
1. An experimental investigation of VTOL lift- engine inlet.
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