Auswahl der wissenschaftlichen Literatur zum Thema „Fan UHBR“
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Zeitschriftenartikel zum Thema "Fan UHBR"
Natale, N., T. Egger, J. Friedrichs und S. Russo. „Aerodynamic Analysis of a scaled UHBR Fan“. IOP Conference Series: Materials Science and Engineering 1226, Nr. 1 (01.02.2022): 012007. http://dx.doi.org/10.1088/1757-899x/1226/1/012007.
Der volle Inhalt der QuellePagès, Valdo, Pierre Duquesne, Stéphane Aubert, Laurent Blanc, Pascal Ferrand, Xavier Ottavy und Christoph Brandstetter. „UHBR Open-Test-Case Fan ECL5/CATANA“. International Journal of Turbomachinery, Propulsion and Power 7, Nr. 2 (31.05.2022): 17. http://dx.doi.org/10.3390/ijtpp7020017.
Der volle Inhalt der QuelleDuquesne, Pierre, Quentin Rendu, Stephane Aubert und Pascal Ferrand. „Choke flutter instability sources tracking with linearized calculations“. International Journal of Numerical Methods for Heat & Fluid Flow 30, Nr. 9 (14.01.2019): 4155–66. http://dx.doi.org/10.1108/hff-06-2018-0281.
Der volle Inhalt der QuellePaletta, N., J. Flüh, J. Lindemann, J. Seume, J. Goessling, J. Friedrichs, T. Eggers et al. „The preliminary design of a scaled Composite UHBR Fan for a wind tunnel test campaign“. IOP Conference Series: Materials Science and Engineering 1226, Nr. 1 (01.02.2022): 012041. http://dx.doi.org/10.1088/1757-899x/1226/1/012041.
Der volle Inhalt der QuelleGoessling, Jan, und Joerg R. Seume. „High-speed Digital Image Correlation (DIC) for measuring deformation and vibration of fast rotating fan blades“. Journal of Physics: Conference Series 2526, Nr. 1 (01.06.2023): 012075. http://dx.doi.org/10.1088/1742-6596/2526/1/012075.
Der volle Inhalt der QuelleEggers, Torben, Jens Friedrichs, Jan Goessling, Joerg R. Seume, Jan Flüh, Jens Lindemann und Nicola Paletta. „Effect of 3D blade design on the aerodynamic, aeroelastic and structural behavior of a scaled UHBR fan“. Journal of Physics: Conference Series 2526, Nr. 1 (01.06.2023): 012032. http://dx.doi.org/10.1088/1742-6596/2526/1/012032.
Der volle Inhalt der QuelleMennicken, M., D. Schoenweitz, M. Schnoes und R. Schnell. „Fan design assessment for BLI propulsion systems“. CEAS Aeronautical Journal 13, Nr. 1 (04.10.2021): 3–19. http://dx.doi.org/10.1007/s13272-021-00532-8.
Der volle Inhalt der QuelleMennicken, M., D. Schoenweitz, M. Schnoes und R. Schnell. „Fan design assessment for BLI propulsion systems“. CEAS Aeronautical Journal 13, Nr. 1 (04.10.2021): 3–19. http://dx.doi.org/10.1007/s13272-021-00532-8.
Der volle Inhalt der QuelleStuermer, Arne. „DLR TAU-Code uRANS Turbofan Modeling for Aircraft Aerodynamics Investigations“. Aerospace 6, Nr. 11 (03.11.2019): 121. http://dx.doi.org/10.3390/aerospace6110121.
Der volle Inhalt der QuelleSchneider, Alexandra P., Benoit Paoletti, Xavier Ottavy und Christoph Brandstetter. „Experimental monitoring of vibrations and the problem of amplitude quantification“. Journal of Physics: Conference Series 2511, Nr. 1 (01.05.2023): 012017. http://dx.doi.org/10.1088/1742-6596/2511/1/012017.
Der volle Inhalt der QuelleDissertationen zum Thema "Fan UHBR"
Schneider, Alexandra Patrizia. „Aerodynamic and aeroelastic investigation of a composite fan for ultra-high-bypass-ratio aircraft engines“. Electronic Thesis or Diss., Ecully, Ecole centrale de Lyon, 2024. http://www.theses.fr/2024ECDL0018.
Der volle Inhalt der QuelleModern low-speed Ultra-High Bypass Ratio (UHBR) fans operate predominantly on the flat part of the compression characteristic, have shorter intake lengths, and employ flexible, lightweight, composite blades. These changes promote the evolution of different types of instabilities with multi-physical interactions such as convective non-synchronous vibration (NSV). To enable further technological ad-vancements, experimental benchmark data on representative geometries required. Within this con-text, the European project CATANA was initiated at Ecole Centrale de Lyon. The open-test-case fan stage ECL5 was designed, following industrial guidelines, and tested experimentally on the facility ECL-B3. This thesis presents the experimental results of the CATANA project. The experimental investiga-tion of the ECL5 reference configuration shows that all design goals have been reached. The machine is operational in a wide range and aerodynamic performance at design condition is exactly coincident with the numerical prediction. In contrast, instability mechanisms are more complex than predicted by the employed numerical methods. Through application of synchronized multi-physical instrumenta-tion, the involved complex fluid-structure interaction is resolved. The analysis of the influence of in-flow conditions and geometrical and structural system symmetry allows to identify the sensitivity of aerodynamic and structural characteristics and the behavior close to the stability limit. The investiga-tion of a second rotor configuration featuring structural mistuning highlights the importance of geo-metrical blade-to-blade variations. They cause an asymmetry of the aerodynamic field at the blade tip and suppress coherently propagating aerodynamic disturbances resulting in a delayed onset of NSV. The results presented in this thesis provide a comprehensive multi-physical characterization of the ECL5 fan stage and serve as a benchmark data set for the validation of numerical simula-tions
Bücher zum Thema "Fan UHBR"
Y, Ho Patrick, Mani Ramani und United States. National Aeronautics and Space Administration., Hrsg. UHB engine fan broadband noise reduction study. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenSteiger, Diego. Zeitreise Time Travel Uhr Kalender 2021: Jahreskalender Für Zeitreise und Science-Fiction Fans. Independently Published, 2020.
Den vollen Inhalt der Quelle findenSteiger, Diego. Zeitreise Time Travel Uhr Studienplaner 2020/21: Semesterplaner Für Zeitreise und Science-Fiction Fans. Independently Published, 2020.
Den vollen Inhalt der Quelle findenNotizbücher, Luftsport. Terminplaner 2019-2020: Für Drachenfliegen Fans Juli 2019 Bis Dezember 2020 Wochentage Unterteilt Von 7. 00 Bis 21. 00 Uhr Mit Den Wichtigsten Feiertagen Deutschlands. Independently Published, 2019.
Den vollen Inhalt der Quelle findenBuchteile zum Thema "Fan UHBR"
Duquesne, Pierre, Stéphane Aubert, Quentin Rendu und Pascal Ferrand. „Effect of Frozen Turbulence Assumption on the Local Blades Vibration on the Choke Flutter Instability in Transonic UHBR Fan“. In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 339–52. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-55594-8_29.
Der volle Inhalt der QuelleKonferenzberichte zum Thema "Fan UHBR"
Eggers, Torben, Jens Friedrichs, Jan Goessling, Joerg R. Seume, Nunzio Natale, Jan Peter Flüh und Nicola Paletta. „Composite UHBR Fan for Forced Response and Flutter Investigations“. In ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/gt2021-58941.
Der volle Inhalt der QuelleBenini, Ernesto, Chetankumar Mistry und Aspi R. Wadia. „Historical Developments in Fan Technologies for Aeroengines“. In ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/gt2023-101639.
Der volle Inhalt der QuelleRodrigues, Martin, Laurent Soulat, Benoit Paoletti, Xavier Ottavy und Christoph Brandstetter. „Aerodynamic Investigation of a Composite Low-Speed Fan for UHBR Application“. In ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/gt2020-14915.
Der volle Inhalt der QuelleZillmann, Jörgen, und U. Tapken. „Tonal Noise Radiation from UHBR Fan - Active Control of Radiation Characteristic“. In 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference). Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-3226.
Der volle Inhalt der QuelleSchuff, Matthias, und Jannik Reisberg. „Flutter Analysis of a Flexible UHBR Fan at Different Flight Conditions“. In ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-76930.
Der volle Inhalt der QuelleBrandstetter, Christoph, Alexandra P. Schneider, Anne-Lise Fiquet, Benoit Paoletti und Xavier Ottavy. „Experiments on Structurally Mistuned UHBR Open-Test-Case Fan ECL5/CATANA“. In ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2024. http://dx.doi.org/10.1115/gt2024-129163.
Der volle Inhalt der QuellePereira, Antonio, Edouard Salze, Josselin Regnard, Fernando Gea-Aguilera und Mathieu Gruber. „New modular fan rig for advanced aeroacoustic tests - Modal decomposition on a 20" UHBR fan stage“. In 25th AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-2604.
Der volle Inhalt der QuelleNeuhaus, Lars, Ulf Tapken, Lars Enghardt, Gerd Enders und Jörgen Zillmann. „Reduction of UHBR fan blade tones by flow induced secondary sound sources“. In 22nd AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-2891.
Der volle Inhalt der QuelleWeckmüller, Christian, Sebastien Guerin und Graham Ashcroft. „CFD/CAA Coupling Applied to DLR UHBR-Fan: Comparison to Experimantal Data“. In 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference). Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-3342.
Der volle Inhalt der QuelleFiquet, Anne-Lise, Alexandra P. Schneider, Benoit Paoletti, Xavier Ottavy und Christoph Brandstetter. „Experiments on Tuned UHBR Open-Test-Case Fan ECL5/CATANA: Stability Limit“. In ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/gt2023-102537.
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