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Aeroacoustic and aerodynamic results (DNW test and DLR numerical simulation) EU HELINOVI (HELIcopter NOise and VIbration Reduction)

Yin, Jianping (2006) Aeroacoustic and aerodynamic results (DNW test and DLR numerical simulation) EU HELINOVI (HELIcopter NOise and VIbration Reduction). Institutskolloquium, Institut für Aerodynamik und Strömungstechnik (AS), 30. Jan. 2006, Braunschweig.

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Document Type:Conference or Workshop Item (Speech)
Title:Aeroacoustic and aerodynamic results (DNW test and DLR numerical simulation) EU HELINOVI (HELIcopter NOise and VIbration Reduction)
Authors:
AuthorsInstitution or Email of Authors
Yin, JianpingUNSPECIFIED
Date:30 January 2006
Page Range:45Folien
Status:Published
Keywords:HeliNOVI , Helicopter Noise and vibration reduction, AEROACOUSTIC MAIN ROTOR/TAIL ROTOR/FUSELAGE ,Tail Rotor NOISE reduction, PIV, Acoustic, Blade pressure, Code validation, Unsteady free wake Panel method (UPM-Mantic), Aeroacoustic code APSIM
Event Title:Institutskolloquium, Institut für Aerodynamik und Strömungstechnik (AS)
Event Location:Braunschweig
Event Type:Other
Event Dates:30. Jan. 2006
Organizer:Institut für Aerodynamik und Strömungstechnik (AS)
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:L VU - Air Traffic and Environment (old)
DLR - Research area:Aeronautics
DLR - Program:L VU - Air Traffic and Environment
DLR - Research theme (Project):L - Quiet Air Traffic (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Dr.-Ing. Jianping Yin
Deposited On:03 Mar 2006
Last Modified:27 Apr 2009 04:59

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