Zobrazeno 1 - 10
of 56
pro vyhledávání: '"Ralf Rudnik"'
Autor:
Sebastian, Spinner, Ralf, Rudnik
Publikováno v:
CEAS Aeronautical Journal; Jan2024, Vol. 15 Issue 1, p49-59, 11p
Publikováno v:
AIAA SCITECH 2023 Forum.
Autor:
Sebastian Spinner, Ralf Rudnik
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA SCITECH 2023 Forum.
Autor:
Ralf Rudnik, F. Lange
Publikováno v:
CEAS Aeronautical Journal. 12:135-146
The Collaborative Research Center 880 is investigating different technologies and configurative variants for the purpose of short take-off and landing (STOL) capabilities, ranging from high-lift systems with Coandӑ flaps to unusual but potentially m
Autor:
Ralf Rudnik, Dennis Keller
Publikováno v:
CEAS Aeronautical Journal. 10:909-924
The scope of this paper is to investigate and improve the aerodynamic properties of a propeller driven state-of-the-art active high-lift configuration in lateral motion. 3D RANS simulations of the landing configuration with circulation control and sl
Autor:
Ralf Rudnik, Dennis Keller
Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783030524289
The aerodynamic properties of a state-of-the-art short take-off and landing aircraft design with circulation control and slipstream deflection in landing configuration have been investigated via RANS simulations. The present paper summarizes the find
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::dc4403381501ee6f697f50c4fbbfe548
https://doi.org/10.1007/978-3-030-52429-6
https://doi.org/10.1007/978-3-030-52429-6
Autor:
Ralf Rudnik, Stefan Melber-Wilkending
Publikováno v:
AIAA Scitech 2020 Forum.
Autor:
Fabian Lange, Ralf Rudnik
Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783030524289
Detailed investigations of interference effects between over-the-wing mounted nacelles (OWN) and airframe were accomplished with the aid of high-fidelity CFD tools on two aircraft configurations. The configurations differ in a variation of the wing p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bd3af872e3c15e5a66c0877d710c4687
https://elib.dlr.de/137900/
https://elib.dlr.de/137900/
Publikováno v:
CEAS Aeronautical Journal. 9:307-317
Experimental aerodynamic investigations of the NASA Common Research Model have been conducted in the NASA Langley National Transonic Facility and the European Transonic Wind Tunnel. Data have been obtained at chord Reynolds numbers of 5, 19.8 and 30