Effects of perpendicular blade-vortex interaction, Part 2: parameter study

AIAA journal

Volumn 37, Issue 7, 1999, Pages 813-817

  Wittmer, K S ^a,c   Devenport, W J ^a   Glegg, S A L ^b  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b FLORIDA ATLANTIC UNIVERSITY   (United States)

^c SIKORSKY AIRCRAFT CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; AIRFOILS; ANEMOMETERS; FLOW MEASUREMENT; MATHEMATICAL MODELS; TURBOMACHINE BLADES; TURBULENT FLOW; VELOCITY MEASUREMENT; VORTEX FLOW; WAKES;

BLADE VORTEX INTERACTION; BLADE VORTEX SEPARATION; BLADE WAKE INTERACTION; STRESS MEASUREMENT; TRAILING EDGE; VELOCITY PROFILES; VORTEX STRENGTH;

FLUID STRUCTURE INTERACTION;

EID: 0033164503     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.7528     Document Type: Article

References (5)

1. Brooks, T. F., Marcolini, M. A., and Pope, D. S., "Main Rotor Broadband Noise Study in the DNW," Journal of the American Helicopter Society, Vol. 34, No. 2, 1989, pp. 3-12.
2. Wittmer, K. S., and Devenport, W. J., "Effects of Perpendicular Blade-Vortex Interaction, Part 1: Turbulence Structure and Development," AIAA Journal, Vol. 37, No. 7, 1999, pp. 805-812.
3. Devenport, W. J., Rife, M. C., Liapis, S. I., and Follin, G. J., "The Structure and Development of a Wing-Tip Vortex," Journal of Fluid Mechanics, Vol. 312, Jan. 1996, pp. 67-106.
4. Glegg, S. A. L., "The Prediction of Blade-Wake Interaction Noise Based on a Turbulent Vortex Model," AIAA Journal, Vol. 29, No. 10, 1991, pp. 1545-1551.
5. Rife, M. C., and Devenport, W. J., "Flow Visualizations of Perpendicular Blade Vortex Interactions," Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Inst. and State Univ., Rept. VPI-AOE-197, Blacksburg, VA, 1993.