On the three-dimensional interaction of a rotor-tip vortex with a cylindrical surface

Journal of Fluid Mechanics

Volumn 425, Issue , 2000, Pages 301-334

  Radcliff, Thomas D ^a   Burggraf, Odus R ^b   Conlisk, A T ^b  

^a UNIVERSITY OF AKRON   (United States)

^b OHIO STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CYLINDER; HELICOPTER; ROTOR; THREE-DIMENSIONAL FLOW; VORTEX;

EID: 0034525942     PISSN: 00221120     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0022112000001981     Document Type: Article

References (22)

1. A model for rotor tip vortex-airframe interaction, Part 1: Theory
2. A model for rotor tip vortex-airframe interaction, Part 2: Comparison with experiment
3. An experimental investigation of the interaction between a model rotor and airframe in forward flight
4. Helicopter rotor wake geometry and its influence in forward flight
5. Calculation of potential flow about arbitrary bodies
6. Evolution of hairpin vortices in a shear flow
7. Summary of the interaction of a rotor wake with a circular cylinder
8. On the impulsive blocking of a vortex-jet
9. Measurement of the interaction between a rotor tip vortex and a cylinder
10. An unsteady helicopter rotor-fuselage aerodynamic interaction analysis
11. 3-D wake measurements near a hovering rotor for determining profile and induced drag
12. Vortex-surface collisions: 3-D core flow effects
13. Recent experiments on vortex collision with a cylinder
14. The motion of a vortex filament with axial flow
15. Axial core flow effects on the interaction of a rotor-tip vortex with an airframe
16. Use of a deformable core vortex model in predicting vortex-surface interactions
17. Computation of a helicopter rotor wake geometry and its influence on rotor harmonic airloads
18. Modern panel method techniques for modeling wake-body interference
19. Theoretical and experimental study of the stability of a vortex pair
20. The boundary layer flow due to a vortex approaching a cylinder