Key Results from a Higher Harmonic Control Aeroacoustic Rotor Test (HART)
暂无分享,去创建一个
W. R. Splettstoesser | F. Micheli | K. Pengel | R. Kube | U. Seelhorst | A. Boutier | Edzard Mercker | W. Wagner | W. Splettstoesser | E. Mercker | F. Micheli | K. Pengel | A. Boutier | R. Kube | W. Wagner | U. Seelhorst
[1] Jay C. Hardin,et al. Concepts for reduction of blade-vortex interaction noise , 1986 .
[2] R. Kube,et al. Automatic Vibration Reduction at a Four-bladed Hingeless Model Rotor - a Wind Tunnel Demonstration. , 1988 .
[3] Thomas F. Brooks,et al. Helicopter main-rotor noise: Determination of source contributions using scaled model data , 1988 .
[4] B. Gmelin,et al. The HART Programme - A Quadrilateral Cooperative Research Effort , 1995 .
[5] R. H. Schlinker,et al. Rotor-vortex interaction noise , 1983 .
[6] Danny R. Hoad. Helicopter blade-vortex interaction locations: Scale-model acoustics and free-wake analysis results , 1987 .
[7] W. R. Splettstoesser,et al. Helicopter Model Rotor-Blade Vortex Interaction Impulsive Noise: Scalability and Parametric Variations , 1984 .
[8] Fredric H. Schmitz,et al. In-Flight Far-Field Measurement of Helicopter Impulsive Noise , 1976 .
[9] W. R. Splettstoesser,et al. Rotor blade-vortex interaction impulsive noise source identification and correlation with rotor wake predictions , 1987 .
[10] W. R. Splettstoesser,et al. Advancing-side directivity and retreating-side interactions of model rotor blade-vortex interaction noise , 1988 .
[11] W. R. Splettstoesser,et al. The HELINOISE Aeroacoustic Rotor Test in the DNW , 1993 .
[12] Kurt Pengel,et al. Flow visualization of helicopter blade tip vortices - A quantitative technique to determine the trajectory and the position of the tip vortex pattern of a model rotor , 1992 .
[13] Matthew L. Wilbur,et al. Reduction of blade-vortex interaction noise through higher harmonic pitch control , 1990 .
[14] C. Cox. Helicopter rotor aerodynamic and aeroacoustic environments , 1977 .
[15] U. Seelhorst,et al. Three Component Laser-Doppler-Velocimeter Development for Large Wind Tunnel , 1993, International Congress on Instrumentation in Aerospace Simulation Facilities,.