Background oriented stereoscopic schlieren (BOSS) for full-scale helicopter vortex characterization
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Markus Raffel | Hugues Richard | Chee Tung | Y. Yu | G.E.A Meier | M. Raffel | G. Meier | C. Tung | H. Richard | Y. Yu
[1] C P Grover,et al. Ground glass differential interferometer. , 1972, Applied optics.
[2] James C. Biggers,et al. Laser velocimeter measurements of the helicopter rotor-induced flow field , 1974 .
[3] Gerd E. A. Meier,et al. Sound produced by vortex-airfoil interaction , 1991 .
[4] W. Merzkirch,et al. Speckle photography of spatially extended refractive-index fields. , 1987, Applied optics.
[5] Gabor T. Herman,et al. Image Reconstruction From Projections , 1975, Real Time Imaging.
[6] Markus Raffel,et al. On the applicability of background oriented optical tomography for large scale aerodynamic investigations , 2000 .
[7] W. R. Splettstoesser,et al. Directivity and prediction of low frequency rotor noise , 1991 .
[8] J. Sullivan,et al. An Experimental Investigation of Vortex Rings and Helicopter Rotor Wakes Using a Laser Doppler Velocimeter , 1973 .
[9] Gabor T. Herman,et al. Image Reconstruction From Projections , 1975, Real Time Imaging.
[10] M. Raffel,et al. Vortical flow structures at a helicopter rotor model measured by LDV and PIV , 1998, The Aeronautical Journal (1968).
[11] M. S. Chandrasekhara,et al. A phase-locked high-speed real-time interferometry system for large amplitude unsteady flows , 1995 .
[12] R. H. Schlinker,et al. Rotor-vortex interaction noise , 1983 .
[13] Jürgen Kompenhans,et al. Instantaneous Flow Field Measurements for Propeller Aircraft and Rotorcraft Research , 2000 .
[14] U. Köpf. Application of speckling for measuring the deflection of laser light by phase objects , 1972 .
[15] Jürgen Kompenhans,et al. Advanced evaluation algorithms for standard and dual plane particle image velocimetry. , 1998 .
[16] G. Meier,et al. New optical tools for fluid mechanics , 1998 .
[17] J. Gordon Leishman,et al. Flow visualization of compressible vortex structures using density gradient techniques , 1993 .
[18] W. R. Splettstoesser,et al. Helicopter Model Rotor-Blade Vortex Interaction Impulsive Noise: Scalability and Parametric Variations , 1984 .
[19] W. R. Splettstoesser,et al. Key Results from a Higher Harmonic Control Aeroacoustic Rotor Test (HART) , 1997 .