An integrated aerodynamic optimization technique based on vortex lattice theory is being proposed. The technique in this work will aim at optimizing the geometric parameters of a general wing with NACA 65-210 airfoil sections under a low speed aerodynamic regime. This will be completed by performing an aerodynamic analysis based on vortex lattice theory with the objective of satisfying a performance index function. This function will seek to optimize the high lift-to-drag ratio of the wing at cruise velocity, while maximizing theoretical cruise range and minimizing wing weight. The optimization method has been developed using MATLAB and the focus of the study will be used by Cirrus Design Corporation and implemented under the panel method software SURFACES as an optimization tool.
","abstract_html":"<p>An integrated aerodynamic optimization technique based on vortex lattice theory is being proposed. The technique in this work will aim at optimizing the geometric parameters of a general wing with NACA 65-210 airfoil sections under a low speed aerodynamic regime. This will be completed by performing an aerodynamic analysis based on vortex lattice theory with the objective of satisfying a performance index function. This function will seek to optimize the high lift-to-drag ratio of the wing at cruise velocity, while maximizing theoretical cruise range and minimizing wing weight. The optimization method has been developed using MATLAB and the focus of the study will be used by Cirrus Design Corporation and implemented under the panel method software SURFACES as an optimization tool.</p>","abstract_has_math":false,"creators":["Pinzon, Santiago"],"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":["Richard P. Anderson","Charles N. Eastlake","R.R. Mankbadi"],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2008,"date_issued":"2008-04-01T07:00:00Z","date_published":"2008-04-01T07:00:00Z","updated_at":"2026-07-27T19:25:45Z","subjects":["wing optimization","vortex lattice theory","Aerodynamics and Fluid Mechanics","Aerospace Engineering"],"languages":[],"rights":[],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"https://commons.erau.edu/db-theses/167","outbound_label":"Repository record","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor","label":"Contributor","values":["Richard P. Anderson","Charles N. Eastlake","R.R. Mankbadi"]},{"key":"dc:creator","label":"Author","values":["Pinzon, Santiago"]}]},{"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":["wing optimization","vortex lattice theory","Aerodynamics and Fluid Mechanics","Aerospace Engineering"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["https://commons.erau.edu/db-theses/167"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description.abstract","label":"Abstract","values":["An integrated aerodynamic optimization technique based on vortex lattice theory is being proposed. The technique in this work will aim at optimizing the geometric parameters of a general wing with NACA 65-210 airfoil sections under a low speed aerodynamic regime. This will be completed by performing an aerodynamic analysis based on vortex lattice theory with the objective of satisfying a performance index function. This function will seek to optimize the high lift-to-drag ratio of the wing at cruise velocity, while maximizing theoretical cruise range and minimizing wing weight. The optimization method has been developed using MATLAB and the focus of the study will be used by Cirrus Design Corporation and implemented under the panel method software SURFACES as an optimization tool.
"]},{"key":"dc:title","label":"Title","values":["Wing Optimization Technique Based on Vortex Lattice Theory"]}]}],"canonical_facts":{"dc:contributor":["Richard P. Anderson","Charles N. Eastlake","R.R. Mankbadi"],"dc:creator":["Pinzon, Santiago"],"dc:description.abstract":["An integrated aerodynamic optimization technique based on vortex lattice theory is being proposed. The technique in this work will aim at optimizing the geometric parameters of a general wing with NACA 65-210 airfoil sections under a low speed aerodynamic regime. This will be completed by performing an aerodynamic analysis based on vortex lattice theory with the objective of satisfying a performance index function. This function will seek to optimize the high lift-to-drag ratio of the wing at cruise velocity, while maximizing theoretical cruise range and minimizing wing weight. The optimization method has been developed using MATLAB and the focus of the study will be used by Cirrus Design Corporation and implemented under the panel method software SURFACES as an optimization tool.
"],"dc:identifier":["https://commons.erau.edu/db-theses/167"],"dc:subject":["wing optimization","vortex lattice theory","Aerodynamics and Fluid Mechanics","Aerospace Engineering"],"dc:title":["Wing Optimization Technique Based on Vortex Lattice Theory"],"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"}