Deflection of Turbofan Exhaust Streams for Enhanced Engine/Nacelle Integration
Author:
Affiliation:
1. Northrop Grumman Corporation, Bethpage, New York 11714
2. Polytechnic University, Farmingdale, New York 11735
3. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2266
Reference5 articles.
1. 3‘‘Thrust Reverser,” Societe Nationale d’Etude et de Construction de Moteurs d’Aviation, Paris, France, Publication, April 1954.
2. 4Abramovich, G. N., The Theory of Turbulent Jets, MIT Press, Cambridge, MA, 1963, pp.365 - 370.
3. Fluidic control of nozzle flow - Some performance measurements
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