A dynamic model for aircraft poststall departure
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.48223
Reference21 articles.
1. Statistical Analysis of General Aviation Stall Spin Accidents
2. Linear analysis of poststall gyrations
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1. High Angle of Attack Aerodynamic Model Identification for Spin Recovery Simulation Using Non-Parametric Smoothing Functions;2018 AIAA Atmospheric Flight Mechanics Conference;2018-01-07
2. An investigation of lateral-directional departure behavior based on yawing–rolling coupled wind tunnel tests;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-08-04
3. Aerodynamic Modeling for Global Stability Analysis;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2002-06-25
4. Simulation of stall, spin, and recovery of a general aviation aircraft;21st Atmospheric Flight Mechanics Conference;1996-07-29
5. Unified development of lateral-directional departure criteria;Journal of Guidance, Control, and Dynamics;1996-03
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