Prediction of wing rock in fixed wing micro aerial vehicles
Author:
Funder
Belt and Road Aerospace Innovation Alliance
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Link
https://link.springer.com/content/pdf/10.1007/s11012-023-01649-2.pdf
Reference40 articles.
1. Nolan RC et al (1992) Wing rock prediction method for a high performance fighter aircraft. Air Force Institute of Tech Wright-Patterson AFB Oh School of Engineering, Columbus
2. Davison MT (1992) An examination of wing rock for the f-15. Air Force Institute of Tech Wright-Patterson AFB Oh School Of Engineering, Columbus
3. Quast T, Nelson R, Fisher D (1991) A study of high alpha dynamics and flow visualization for a 2.5-percent model of the f-18 HARV undergoing wing rock. 9th Appl Aerodyn Conf. https://doi.org/10.2514/6.1991-3267
4. Arena AJR, Nelson R (1989) The effect of asymmetric vortex wake characteristics on a slender delta wing undergoing wing rock motion. 16th Atmos Flight Mech Conf. https://doi.org/10.2514/6.1989-3348
5. Arena AS Jr, Nelson RC (1994) Experimental investigations on limit cycle wing rock of slender wings. J Aircr 31(5):1148–1155. https://doi.org/10.2514/3.46625
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