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AEROACOUSTIC TEST RESULTS FROM HELINOVI MAIN ROTOR/TAIL ROTOR/FUSELAGE TEST IN DNW

Yin, Jianping (2006) AEROACOUSTIC TEST RESULTS FROM HELINOVI MAIN ROTOR/TAIL ROTOR/FUSELAGE TEST IN DNW. Other.

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Document Type:Monograph (Other)
Title:AEROACOUSTIC TEST RESULTS FROM HELINOVI MAIN ROTOR/TAIL ROTOR/FUSELAGE TEST IN DNW
Authors:
AuthorsInstitution or Email of Authors
Yin, JianpingUNSPECIFIED
Date:March 2006
Series Name:STAB Jahresbericht 2005 (Mitteilung), Arbeitsgemeinschaft ‘ Strömungen mit Ablösung’pp68-69
Status:Published
Keywords:Helinovi,Helicopter Noise & Vibration Reduction, main rotor / tail rotor interference,tail rotor noise reduction potentials, DNW wind tunnel test, acoustic inflow and outflow microphones, blade pressure, Particle Image Velocimetry (PIV).
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Quiet and Comfortable Rotorcraft
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Dr.-Ing. Jianping Yin
Deposited On:15 Jan 2007
Last Modified:27 Apr 2009 13:25

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