Angular Momentum Control in Nonlinear Flight
Author:
Affiliation:
1. Wichita State University, Wichita, Kansas 67260-0044
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2618
Reference16 articles.
1. National Transportation Safety Board, “Annual Review of Aircraft Accident Data,” PB94-181054 or NTSB/ARG-94/02.
2. Statistical Analysis of General Aviation Stall Spin Accidents
3. Reduction of Stall-Spin Entry Tendencies Through Wing Aerodynamic Design
4. An Iterative Non-Linear Lifting Line Model For Wings with Unsymmetrical Stall
5. Numerical lifting line theory applied to drooped leading-edge wings below and above stall
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1. A review and historical development of analytical techniques to predict aircraft spin and recovery characteristics;Aircraft Engineering and Aerospace Technology;2020-07-13
2. Post-Stall Motions Evolving Toward Chaos;Journal of Aircraft;2007-05
3. Momentum Vector Control for Spin Recovery;Journal of Aircraft;2004-11
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