Nonlinear Rate and Amplitude Effects on a Generic Combat Aircraft Model
Author:
Affiliation:
1. Institute for Aerospace Research, Ottawa, Ontario K1A 0R6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2608
Reference21 articles.
1. Wind-Tunnel Aerodynamics in Rotary Tests of Combat Aircraft Models
2. Vortex Characteristics of Pitching Double-Delta Wings
3. Approximate Nonlinear Slender Wing Aerodynamics
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