The Higher-Harmonic Control Aeroacoustic Rotor Test (HART) in the DNW-LLF
Abstract
With increasing use of helicopters the problem of noise emission of helicopters became more and more important. The first HART program on rotorcraft noise has shown that blade vortex interaction (BVI) is a major source of impulsive noise. As BVI-noise is generated by the induced velocities of tip vortices, it depends on vortex strength and miss-distance, which itself depends on vortex location and orientation and convection speed relative to the path of the advancing blade. The detailed study of these vortices by means of Particle Image Velocimetry (PIV) and by means of flow visualization with the Laser Light Sheet method (LLS) is of particular interest for progress towards quieter rotorcraft and is the subject of this program. For a detailed analysis of blade vortex interaction it is also essential to gain some knowledge about the deformation of the rotor blades due to aerodynamic loading at different azimuth angles. For this purpose DNW developed a dedicated photonical method to evaluate blade deflection during operation of the rotor.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 2000
- Accession Number
- ADA389689
Entities
People
- E. Merker
- G. Lehmann
- K. Pengel