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Full Fairing Rotor Head Aerodynamic Design Optimization

Resultado final

Project webpage accessible to the public

Starting the date for the web presence of the project which will be continuously updated according to the progress during the project.

Dissemination and methodology report

Report on methodology and numerical approach with respect to the final project results and dissemination.

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Publicaciones

Performance improvement of a compound helicopter rotor head by aerodynamic shape optimization

Autores: P. Pölzlbauer, D. Desvigne, C. Breitsamter
Publicado en: 31st Congress of the International Council of the Aeronautical Sciences, Every two years, 2018
Editor: International Council of the Aeronautical Sciences

Aerodynamic Design Optimization of a Helicopter Rotor Blade-Sleeve Fairing

Autores: P. Pölzlbauer (1), D. Desvigne (2), C. Breitsamter (1) (1) Technical University of Munich, Department of Mechanical Engineering, Chair of Aerodynamics and Fluid Mechanics, Germany (2) Airbus Helicopters, France
Publicado en: Proceedings of the German Aerospace Congress, Annually, 2017
Editor: Deutsche Gesellschaft für Luft- und Raumfahrt Lilienthal-Oberth e.V.

Aerodynamic design optimization of a helicopter rotor blade-sleeve fairing

Autores: P. Pölzlbauer, D. Desvigne, C. Breitsamter
Publicado en: CEAS Aeronautical Journal, 2018, ISSN 1869-5582
Editor: Springer Science + Business Media
DOI: 10.1007/s13272-018-0341-0

Performance improvement of a compound helicopter rotor head by aerodynamic design optimisation of a blade-sleeve fairing

Autores: P. Pölzlbauer, C. Breitsamter, D. Desvigne
Publicado en: The Aeronautical Journal, 2019, Page(s) 1-20, ISSN 0001-9240
Editor: Royal Aeronautical Society
DOI: 10.1017/aer.2018.172