Three-dimensional tracking of lesion profile during laser surgery based on shock wave detection

2014 ◽  
Author(s):  
Erwin Bay ◽  
Xosé Luis Dean Ben ◽  
Genny A. Pang ◽  
Alexandre Douplik ◽  
Daniel Razansky
Keyword(s):  
Shock Wave ◽  
Laser Surgery ◽  
Three Dimensional ◽  
Wave Detection ◽  
Lesion Profile

Three-Dimensional Shock Wave Detection Based on the Theory of Characteristics

AIAA Journal ◽  
2013 ◽  
Vol 51 (9) ◽  
pp. 2126-2132 ◽  
Author(s):  
Masashi Kanamori ◽  
Kojiro Suzuki
Keyword(s):  
Shock Wave ◽  
Three Dimensional ◽  
Wave Detection

Real-time monitoring of incision profile during laser surgery using shock wave detection

2013 ◽  
Vol 8 (1-2) ◽  
pp. 102-111 ◽  
Author(s):  
Erwin Bay ◽  
Xosé Luís Deán-Ben ◽  
Genny A. Pang ◽  
Alexandre Douplik ◽  
Daniel Razansky
Keyword(s):  
Shock Wave ◽  
Real Time ◽  
Laser Surgery ◽  
Real Time Monitoring ◽  
Wave Detection

Unsteady Three-Dimensional Analysis of Inlet Distortion in a Transonic Fan

2006 ◽  
Author(s):  
Peng Sun ◽  
Guotal Feng
Keyword(s):  
Shock Wave ◽  
Total Pressure ◽  
Large Scale ◽  
Three Dimensional ◽  
Navier Stokes ◽  
Inlet Distortion ◽  
Flow Loss ◽  
Large Scale Vortex ◽  
Total Temperature ◽  
Transonic Fan

A time-accurate three-dimensional Navier-Stokes solver of the unsteady flow field in a transonic fan was carried out using "Fluent-parallel" in a parallel supercomputer. The numerical simulation focused on a transonic fan with inlet square wave total pressure distortion and the analysis of result consisted of three aspects. The first was about inlet parameters redistribution and outlet total temperature distortion induced by inlet total pressure distortion. The pattern and causation of flow loss caused by pressure distortion in rotor were analyzed secondly. It was found that the influence of distortion was different at different radial positions. In hub area, transportation-loss and mixing-loss were the main loss patterns. Distortion not only complicated them but enhanced them. Especially in stator, inlet total pressure distortion induced large-scale vortex, which produced backflow and increased the loss. While in casing area, distortion changed the format of shock wave and increased the shock loss. Finally, the format of shock wave and the hysteresis of rotor to distortion were analyzed in detail.

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