Unsteady Wing-Pylon-Nacelle Interference in Transonic Flow
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.31363
Reference27 articles.
1. Flutter stability of annular wings in incompressible flow
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4. Measurement of unsteady airloads on an oscillating engine and a wing/engine combination
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