Unsteady and Post-Stall Model Identification Using Dynamic Stall Maneuvers
Author:
Affiliation:
1. Brazilian Air Force
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2705
Reference11 articles.
1. 1Federal Aviation Administration, Advisory Circular AC 25-7C: “Flight Test Guide for Certification of Transport Category Airplanes. Date: 10/16/12.
2. Partitioning of flight data for aerodynamic modeling of aircraft at high angles of attack
3. X-31A system identification using single-surface excitation at high angles of attack
4. Determination of nonlinear aerodynamic coefficients using the estimation-before-modeling method
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