Predicting the Contribution of Running Propellers to Aircraft Stability Derivatives
Author:
Affiliation:
1. Utah State University, Logan, Utah 84322-4130
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.7221
Reference17 articles.
Cited by 16 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Aerodynamic Performance and Static Stability Characteristics of Aircraft with Tail-Mounted Propellers;Journal of Aircraft;2021-11-15
2. Development of an Unsteady Vortex Lattice Method to Model Propellers at Incidence;AIAA Journal;2021-09-28
3. Design optimization of multi-objective proportional–integral–derivative controllers for enhanced handling quality of a twin-engine, propeller-driven airplane;Advances in Mechanical Engineering;2020-06
4. Propeller modeling approaches for off–design operative conditions;Ocean Engineering;2019-04
5. Experimental and Numerical Investigation of Propeller Loads in Off-Design Conditions;Journal of Marine Science and Engineering;2018-04-24
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