Wing and airfoil geometry x 365/29/2023 ![]() ![]() The salient features of MAVs have resulted in the establishment of some researches toward the optimization and enhancement of such planes. Depending on the mission type, dimensions of the equipment vary. fixed wing, VTOL, flapping wing, and rotary wing. They could be designed in four types, i.e. Unmanned airplanes smaller than 500 mm and weighing less than 500 g are considered as micro air vehicle (MAV). After the design, steps of manufacturing will be started. The final step of design is the optimization of the micro air vehicle for increasing its performance and endurance. Next step is selection of electric equipment such as motor, batteries, servo, etc. After calculation of the control surfaces, the designed micro air vehicle is analyzed in XFLR5 software. The results of these processes are determination of surfaces, dimensions and airfoils of the tails and center of gravity of the plane. Then micro air vehicle and aerodynamic center of wing are calculated and stability equations for micro air vehicle are simulated. Next step is designing the fuselage for the airplane. After this stage, the wing of micro air vehicle is designed completely and analysis is carried out to determine the aerodynamics coefficients. After determination of the planform geometry, selection of the airfoil is carried out by complying with the defined criteria. Completion of these four phases results in the specification of the geometry and dimensions of the wing in an optimum manner. In this method, the sizing process is started simultaneously, which involves the following cases: specification of mission and aviation plan determination of planform and aspect ratio constraint analysis estimation of plane weight. The main aim of the cycle is to decrease the designing time for an optimum design. The idea is to propose a complete cycle containing all micro air vehicles design subjects such as aerodynamics, stability, structure, and navigation. This study attempts to present a new and comprehensive cycle for the design of fixed wing micro air vehicles. All subjects Allied Health Cardiology & Cardiovascular Medicine Dentistry Emergency Medicine & Critical Care Endocrinology & Metabolism Environmental Science General Medicine Geriatrics Infectious Diseases Medico-legal Neurology Nursing Nutrition Obstetrics & Gynecology Oncology Orthopaedics & Sports Medicine Otolaryngology Palliative Medicine & Chronic Care Pediatrics Pharmacology & Toxicology Psychiatry & Psychology Public Health Pulmonary & Respiratory Medicine Radiology Research Methods & Evaluation Rheumatology Surgery Tropical Medicine Veterinary Medicine Cell Biology Clinical Biochemistry Environmental Science Life Sciences Neuroscience Pharmacology & Toxicology Biomedical Engineering Engineering & Computing Environmental Engineering Materials Science Anthropology & Archaeology Communication & Media Studies Criminology & Criminal Justice Cultural Studies Economics & Development Education Environmental Studies Ethnic Studies Family Studies Gender Studies Geography Gerontology & Aging Group Studies History Information Science Interpersonal Violence Language & Linguistics Law Management & Organization Studies Marketing & Hospitality Music Peace Studies & Conflict Resolution Philosophy Politics & International Relations Psychoanalysis Psychology & Counseling Public Administration Regional Studies Religion Research Methods & Evaluation Science & Society Studies Social Work & Social Policy Sociology Special Education Urban Studies & Planning BROWSE JOURNALS ![]()
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