Transonic Flutter Analysis of a Rectangular Wing with Conventional Airfoil Sections
Author:
Affiliation:
1. Air Force Flight Dynamics Laboratory, Wright-Patterson AFB, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50866
Reference14 articles.
1. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.
2. AN IMPROVED MACH-BOX APPROACH FOR THE CALCULATION OF SUPERSONIC OSCILLATORY PRESSURE DISTRIBUTIONS
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