Break-up and atomization characteristics of JetA liquid fuel were investigated numerically. The results have been compared to various experimental results to evaluate the accuracy of the numerical model. The CFD code ANSYS-CFX 12.0 was used to carry out the steady state analysis at different time scales. A comparison between the atomization characteristics of a pressure jet atomizer and an air-blast atomizer is shown. By employing a Lagrangian particle tracking method to track the path of the liquid particles, the liquid jet/spray phenomena was studied in light of low and high back pressure environments. The 'BLOB' primary atomization model and the Cascade Atomization and Breakup model 'CAB' which is an extension of the Enhanced Taylor Analogy Breakup model 'ETAB' was incorporated for analyzing the secondary breakup. Parameters taken into consideration were the JetA liquid particle traveling time and distance, Sauter Mean Diameter, Weber number, JetA Liquid Average Velocity and the turbulence kinetic energy.
","abstract_html":"<p>Break-up and atomization characteristics of JetA liquid fuel were investigated numerically. The results have been compared to various experimental results to evaluate the accuracy of the numerical model. The CFD code ANSYS-CFX 12.0 was used to carry out the steady state analysis at different time scales. A comparison between the atomization characteristics of a pressure jet atomizer and an air-blast atomizer is shown. By employing a Lagrangian particle tracking method to track the path of the liquid particles, the liquid jet/spray phenomena was studied in light of low and high back pressure environments. The 'BLOB' primary atomization model and the Cascade Atomization and Breakup model 'CAB' which is an extension of the Enhanced Taylor Analogy Breakup model 'ETAB' was incorporated for analyzing the secondary breakup. Parameters taken into consideration were the JetA liquid particle traveling time and distance, Sauter Mean Diameter, Weber number, JetA Liquid Average Velocity and the turbulence kinetic energy.</p>","abstract_has_math":false,"creators":["Bhatt, Yash Akhil"],"institution":null,"degree_name":"Master of Science in Aerospace Engineering","degree_level":"Thesis - Open Access","degree_discipline":"Aerospace Engineering","degree_department":null,"school":null,"contributors":["R.R. Mankbadi","Bereket Berhane"],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2010,"date_issued":"2010-04-01T07:00:00Z","date_published":"2010-04-01T07:00:00Z","updated_at":"2026-07-27T19:25:45Z","subjects":["numerical simulation","liquid jet","atomization","ANSYS","Aerodynamics and Fluid Mechanics","Aerospace Engineering"],"languages":[],"rights":[],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"https://commons.erau.edu/db-theses/26","outbound_label":"Repository record","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor","label":"Contributor","values":["R.R. Mankbadi","Bereket Berhane"]},{"key":"dc:creator","label":"Author","values":["Bhatt, Yash Akhil"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"thesis:degree_discipline","label":"Discipline","values":["Aerospace Engineering"]},{"key":"thesis:degree_level","label":"Degree Level","values":["Thesis - Open Access"]},{"key":"thesis:degree_name","label":"Degree Name","values":["Master of Science in Aerospace Engineering"]}]},{"id":"subjects_keywords","label":"Subjects and Keywords","entries":[{"key":"dc:subject","label":"Dc Subject","values":["numerical simulation","liquid jet","atomization","ANSYS","Aerodynamics and Fluid Mechanics","Aerospace Engineering"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["https://commons.erau.edu/db-theses/26"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description.abstract","label":"Abstract","values":["Break-up and atomization characteristics of JetA liquid fuel were investigated numerically. The results have been compared to various experimental results to evaluate the accuracy of the numerical model. The CFD code ANSYS-CFX 12.0 was used to carry out the steady state analysis at different time scales. A comparison between the atomization characteristics of a pressure jet atomizer and an air-blast atomizer is shown. By employing a Lagrangian particle tracking method to track the path of the liquid particles, the liquid jet/spray phenomena was studied in light of low and high back pressure environments. The 'BLOB' primary atomization model and the Cascade Atomization and Breakup model 'CAB' which is an extension of the Enhanced Taylor Analogy Breakup model 'ETAB' was incorporated for analyzing the secondary breakup. Parameters taken into consideration were the JetA liquid particle traveling time and distance, Sauter Mean Diameter, Weber number, JetA Liquid Average Velocity and the turbulence kinetic energy.
"]},{"key":"dc:title","label":"Title","values":["Numerical Simulation of a Liquid Jet Atomization and Break-Up Using ANSYS-CFX 12.0"]}]}],"canonical_facts":{"dc:contributor":["R.R. Mankbadi","Bereket Berhane"],"dc:creator":["Bhatt, Yash Akhil"],"dc:description.abstract":["Break-up and atomization characteristics of JetA liquid fuel were investigated numerically. The results have been compared to various experimental results to evaluate the accuracy of the numerical model. The CFD code ANSYS-CFX 12.0 was used to carry out the steady state analysis at different time scales. A comparison between the atomization characteristics of a pressure jet atomizer and an air-blast atomizer is shown. By employing a Lagrangian particle tracking method to track the path of the liquid particles, the liquid jet/spray phenomena was studied in light of low and high back pressure environments. The 'BLOB' primary atomization model and the Cascade Atomization and Breakup model 'CAB' which is an extension of the Enhanced Taylor Analogy Breakup model 'ETAB' was incorporated for analyzing the secondary breakup. Parameters taken into consideration were the JetA liquid particle traveling time and distance, Sauter Mean Diameter, Weber number, JetA Liquid Average Velocity and the turbulence kinetic energy.
"],"dc:identifier":["https://commons.erau.edu/db-theses/26"],"dc:subject":["numerical simulation","liquid jet","atomization","ANSYS","Aerodynamics and Fluid Mechanics","Aerospace Engineering"],"dc:title":["Numerical Simulation of a Liquid Jet Atomization and Break-Up Using ANSYS-CFX 12.0"],"thesis:degree_discipline":["Aerospace Engineering"],"thesis:degree_level":["Thesis - Open Access"],"thesis:degree_name":["Master of Science in Aerospace Engineering"]},"updated_at":"2026-07-27T19:25:45Z"}