Survey of inlet development for supersonic aircraft
Author:
Affiliation:
1. USAF, Wright Aeronautical Laboratories, Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-1164
Reference37 articles.
1. Installation Handbook for Turbojet Engines, Ch. 8, "Induction Systemst',published by G. E., 1952.
2. Airframe-Propulsion Integration for Fighter Aircraft
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1. Numerical Analysis of Effect of Boundary Layer Characteristics on the Flow Field in S-shaped Inlet;MATEC Web of Conferences;2015
2. A Ground Test Method and the Error Analysis of the Heat Exchanger in the Intake of Aircraft;Advanced Materials Research;2014-09
3. Canonical Normal Shock Wave/Boundary-Layer Interaction Flows Relevant to External Compression Inlets;AIAA Journal;2013-09
4. Shock Wave/Boundary-Layer Interaction Control Using a Combination of Vortex Generators and Bleed;AIAA Journal;2013-05
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