Subcritical damping ratios of a two-dimensional airfoil in transonic flow
Author:
Affiliation:
1. National Research Council Canada, Ottawa, Ontario, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45210
Reference35 articles.
1. l, L. J. "Response of Flight Vehicles to Nonstationary Random Atmospheric Turbulent," Ph.D. Dissertation, University of Illinois at Urbana-Champaign,1970, UniversityMicrofilms, Ann Arbor, MI, (127 pp.).
2. Response of Flight Vehicles to Nonstationary Atmospheric Turbulence
3. Analysis of airplane response to nonstationary turbulence including wing bending flexibility. II.
4. Response of a rigid aircraft to nonstationary atmospheric turbulence.
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