Experimental Propeller Performance Analysis on a Large Scale Distributed Propulsion Configuration at High Lift
Author:
Affiliation:
1. Institute of Jet Propulsion and Turbomachinery, Technical University Braunschweig
2. Institute for Fluid Mechanics, Technical University Braunschweig
Publisher
Gas Turbine Society of Japan
Link
https://www.jstage.jst.go.jp/article/jgpp/15/1/15_vol15no1tp05/_pdf
Reference11 articles.
1. Kim, H. D., A. T. Perry, and P. J. Ansell. July 9, 2018. “A Review of Distributed Electric Propulsion Concepts for Air Vehicle Technology”. In: 2018 AIAA/IEEE Electric Aircraft Technologies Symposium. Cincinnati, Ohio: American Institute of Aeronautics and Astronautics. ISBN: 978-1-62410-572-2. DOI: 10.2514/6.2018-4998.
2. Deere, K. A., S. Viken, M. Carter, J. K. Viken, M. Wiese, and N. Farr. Jan. 1, 2017. “Computational Analysis of Powered Lift Augmentation for the LEAPTech Distributed Electric Propulsion Wing”. In: 35th AIAA Applied Aerodynamics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics. ISBN: 978-1-62410-501-2. DOI: 10.2514/6.2017-3921.
3. Vries, R. de, N. van Arnhem, T. Sinnige, R. Vos, and L. L. Veldhuis. Nov. 2021. “Aerodynamic interaction between propellers of a distributed-propulsion system in forward flight”. In: Aerospace Science and Technology 118, p. 107009. DOI: 10.1016/j.ast.2021.107009.
4. Rosa, D. de, E. M. Tirado, and G. Mingione. Mar. 2022. “Parametric Investigation of a Distributed Propulsion System on a Regional Aircraft”. In: Aerospace 9.4, p. 176. DOI: 10.3390/aerospace9040176.
5. Duivenvoorden, R., N. Suard, T. Sinnige, and L. L. Veldhuis. June 27, 2022. “Experimental Investigation of Aerodynamic Interactions of aWing with Deployed Fowler Flap under Influence of a Propeller Slipstream”. In: AIAA AVIATION 2022 Forum. AIAA AVIATION 2022 Forum. Chicago, IL & Virtual: American Institute of Aeronautics and Astronautics. ISBN: 978-1-62410-635-4. DOI: 10.2514/6.2022-3216.
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