TRABECULAR BONE REMODELING AFTER LATERAL LUMBAR INTERBODY FUSION: INDIRECT FINDINGS FOR STRESS TRANSMISSION BETWEEN VERTEBRAE AFTER SPINAL FUSION SURGERY

Trabecular Bone Remodeling after Lateral Lumbar Interbody Fusion: Indirect Findings for Stress Transmission between Vertebrae after Spinal Fusion Surgery

Introduction: After posterior lumbar interbody fusion (PLIF), trabecular bone remodeling (TBR) occurs in the vertebral body.This study aimed to investigate whether imaging findings obtained with PLIF are applicable to lateral lumbar interbody fusion (LLIF).Methods: A total of 53 cases who underwent one- or two-level LLIF with polyether ether ketone

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Addition of Organic Acids and Lactobacillus acidophilus to the Leguminous Forage Chamaecrista rotundifolia Improved the Quality and Decreased Harmful Bacteria of the Silage

This study aimed to investigate the effects of citric acid, malic acid, and Lactobacillus acidophilus (L) on fermentation parameters and the microbial community of leguminous Chamaecrista rotundifolia silage.Fresh C.rotundifolia was treated without any additive (CK), or with L (106 CFU/g fresh weight), different levels (0.1, 0.3, 0.5, and 1% fresh

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Power Quality Improvement in Commercial and Industrial Sites: An Integrated Approach Mitigating Power Oscillations

This paper introduces a novel control strategy for multifunctional grid-tied inverters in industrial/commercial power systems, aiming to address the compensation of instantaneous power oscillations.The proposed strategy is derived from the Conservative Power Theory, which offers the ability to extract and analyze oscillating power terms directly in

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A Cost-Effective Tracking Algorithm for Hypersonic Glide Vehicle Maneuver Based on Modified Aerodynamic Model

In order to defend the hypersonic glide vehicle (HGV), a cost-effective single-model tracking algorithm using Cubature Kalman filter (CKF) is proposed Table in this paper based on modified aerodynamic model (MAM) as process equation and radar measurement model as measurement equation.In the existing aerodynamic model, the two control variables atta

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