scholarly journals Single-stage decompression of C1–D9 anterior epidural abscess by a gas-producing enteric pathogen

2021 ◽  
Vol 4 (2) ◽  
pp. 260
Author(s):  
MAtharsh Chander ◽  
Vetri Nallathambi
2004 ◽  
Vol 17 (6) ◽  
pp. 1-5 ◽  
Author(s):  
Alfred T. Ogden ◽  
Michael G. Kaiser

Surgical intervention is indicated for pyogenic vertebral discitis and osteomyelitis in patients in whom medical therapy has failed, and in those with neurological compromise, mechanical instability, epidural abscess, or intractable pain. Surgical management has evolved to include single-stage operations for debridement and stabilization as well as more aggressive reconstruction strategies with respect to instrumentation. A review of the literature demonstrates excellent outcomes with single-stage operations and placement of hardware wherever it is required. Using this method, the authors have treated 16 patients without a single incidence of recurrent infection or hardware failure after almost 2 years of follow up.


2007 ◽  
Vol 177 (4S) ◽  
pp. 12-12
Author(s):  
L. Andrew Evans ◽  
Benjamin Moses ◽  
Kevin Rice ◽  
Craig Robson ◽  
Allen F. Morey

1989 ◽  
Vol 50 (C1) ◽  
pp. C1-813-C1-817
Author(s):  
M. ARNOULD ◽  
F. BAETEN ◽  
D. DARQUENNES ◽  
Th. DELBAR ◽  
C. DOM ◽  
...  

2014 ◽  
Vol 75 (S 01) ◽  
Author(s):  
Sherif Emara ◽  
Hassan Nablsi ◽  
Tarek ELKammash ◽  
Mohamed Sief ◽  
Khaled Attia ◽  
...  
Keyword(s):  

Author(s):  
Kyu-Sup Cho ◽  
Dae-Woon Kang ◽  
Chang-Hun Lee ◽  
Hwan-Jung Roh

2020 ◽  
Vol 14 (4) ◽  
pp. 7369-7378
Author(s):  
Ky-Quang Pham ◽  
Xuan-Truong Le ◽  
Cong-Truong Dinh

Splitter blades located between stator blades in a single-stage axial compressor were proposed and investigated in this work to find their effects on aerodynamic performance and operating stability. Aerodynamic performance of the compressor was evaluated using three-dimensional Reynolds-averaged Navier-Stokes equations using the k-e turbulence model with a scalable wall function. The numerical results for the typical performance parameters without stator splitter blades were validated in comparison with experimental data. The numerical results of a parametric study using four geometric parameters (chord length, coverage angle, height and position) of the stator splitter blades showed that the operational stability of the single-stage axial compressor enhances remarkably using the stator splitter blades. The splitters were effective in suppressing flow separation in the stator domain of the compressor at near-stall condition which affects considerably the aerodynamic performance of the compressor.


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