International Research in Engineering - December 2022

The topics in the book as follows ;

USE OF WEARABLE TECHNOLOGIES IN DIFFERENT AREAS
POLYMERS USED IN THE TEXTILE COATING INDUSTRY, THEIR APPLICATIONS AND THEIR EFFECTS ON HUMAN HEALTH
THE ROLE OF BUILDING CONTROL FIRMS IN REDUCTION OF OCCUPATIONAL ACCIDENTS IN THE CONSTRUCTION SECTOR
COMPARISON OF GEOGRAPHICAL INFORMATION SYSTEMS (GIS) WITH INTELLIGENCE TRANSPORTATION SYSTEM (ITS) IN INDIA AND JAPAN
DETECTION OF SHIPS USING SENTINEL-1 SYNTHETIC APERTURE RADAR IMAGES
Discriminating of Essential Tremor and Parkinson's Disease Using Frequency Analysis Method
Blood Glucose Prediction from Nondiabetic and Diabetic Exhaled Breath via Machine Learning
A REVIEW OF NATURAL SYSTEMS FOR WASTEWATER TREATMENT
Producing Light Concretes by Using Agricultural Waste of Rice
AN OVERVIEW OF MICROWAVE NONDESTRUCTIVE TESTING (NDT) METHOD
INVESTIGATION OF RAINWATER HARVESTING IN A FACTORY LOCATED IN KÜTAHYA-TURKEY
EVALUATION OF PERFORMANCE OF EARTHQUAKE PARAMETERS BY MACHINE LEARNING (CASE OF STUDY CENTRAL ANATOLIA REGION)
Modification of Fly Ash Supplemented Cement-Based Composites with Nanomaterials
Using blended learning in textile engineering education, an example of internship class
Role of Internet of Things in Supply Chain Management
APPLICATION OF THE ELMERI SAFETY INDEX METHOD TO SOME CONSTRUCTIONS IN THE ÇORUM REGION TO IMPROVE THE RESPONSIBILITIES OF BUILDING CONTROL FIRMS IN TERMS OF OCCUPATIONAL HEALTH AND SAFETY
Digital Transformation Based on SWOT Analysis for the Widespread Use of Machine Learning Methods in Construction Project Management
ELECTRICAL CIRCUIT THEOREMS AND SIMULINK ANALYSIS
ANALYSIS OF UNIFORM FRAMES UNDER HORIZONTAL LOADS
Condition Matrix Via Null Space and Singular Value Decomposition in Integrated Force Method To Analyze Space Truss
AUTONOMOUS CAGE MODEL
SLUDGE DISINTEGRATION METHODS TO ENHANCE ANAEROBIC DIGESTION: AN UP TO DATE REVIEW
RESONANCE IN ELECTRICAL CIRCUITS
RECOMMENDATION OF EIGHT ROTOR UAVS WITH DIFFERENT CONFIGURATIONS AND COMPARISON OF FLIGHT PERFORMANCES WITH TWO DIFFERENT UAVS WITH STANDARD CONFIGURATIONS UNDER IMPACT FORCE