Numerical Methods and Experimental Means for the Integration of Future Propulsion Systems
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Numerical Methods and Experimental Means for the Integration of Future Propulsion Systems
A Resume of the Achievements Made within the CleanSky 2 XDC Demonstrator
Boden, Fritz
Springer International Publishing AG
04/2026
288
Dura
Inglês
9783031977244
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Introduction.- The XDC - an Overview on the CleanSky 2 Demonstrator on Common Numerical Methods and Experimental Means.- Numerical Methods.- Hybrid wing body as a low-noise aircraft from a multidisciplinary point of view.- Fast prediction of fan broadband noise with an analytical aerodynamic model suited for transonic rotor blades.- Design and Integration of UHBR Propulsion Systems - An Overview of DLR Activities within the Clean Sky 2 ASPIRE and SA (2)FIR Projects.- Structural Design of a Generic High Bypass Ratio Fan.- Parametric Structural Modelling for Aeroelastic and Aeroacoustic Analyses of an Aircraft Fuselage.- Flutter Assessment of a Passenger Aircraft with Standard and UHBR Engines.- Experimental Means.- Temperature-Sensitive Paint Method for the Investigation of Stationary Crossflow Instability Induced Boundary Layer Transition.- Improving source localization with SODIX for far-field measurements in static engine noise tests.- Experimental Vibroacoustic Characterization of an A320 Wing Utilizing a Controlled Shaker System for Artificial Engine-Vibration Excitation.- Full Scale Particle Image Velocimetry in Aircraft Related Flows Under Open-Air Conditions.- 3D Lagrangian Particle Tracking with Shake-The-Box Applied to Large-Volume Measurements.
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T-Tail Flutter;vibration testing;UHBR propulsion systems;Aircraft Rear Fuselage;transonic rotor blades;engine noise tests;aeroacoustics;MEMS microphones;Particle Image Velocimetry;Aeroelastic Analysis;DLR
Introduction.- The XDC - an Overview on the CleanSky 2 Demonstrator on Common Numerical Methods and Experimental Means.- Numerical Methods.- Hybrid wing body as a low-noise aircraft from a multidisciplinary point of view.- Fast prediction of fan broadband noise with an analytical aerodynamic model suited for transonic rotor blades.- Design and Integration of UHBR Propulsion Systems - An Overview of DLR Activities within the Clean Sky 2 ASPIRE and SA (2)FIR Projects.- Structural Design of a Generic High Bypass Ratio Fan.- Parametric Structural Modelling for Aeroelastic and Aeroacoustic Analyses of an Aircraft Fuselage.- Flutter Assessment of a Passenger Aircraft with Standard and UHBR Engines.- Experimental Means.- Temperature-Sensitive Paint Method for the Investigation of Stationary Crossflow Instability Induced Boundary Layer Transition.- Improving source localization with SODIX for far-field measurements in static engine noise tests.- Experimental Vibroacoustic Characterization of an A320 Wing Utilizing a Controlled Shaker System for Artificial Engine-Vibration Excitation.- Full Scale Particle Image Velocimetry in Aircraft Related Flows Under Open-Air Conditions.- 3D Lagrangian Particle Tracking with Shake-The-Box Applied to Large-Volume Measurements.
Este título pertence ao(s) assunto(s) indicados(s). Para ver outros títulos clique no assunto desejado.
