Performance Analysis of a Drone Propeller by Analytical and Numerical Methods

A tétel rövid nézete
dc.contributor.advisorSzodrai, Ferenc
dc.contributor.authorKaspapettai Kuppusamy, Naveen
dc.contributor.departmentDE--Műszaki Kar
dc.date.accessioned2025-02-05T12:30:55Z
dc.date.available2025-02-05T12:30:55Z
dc.date.created2024-11-25
dc.description.abstractThis study focuses on calculation the aerodynamic forces of a small quadcopter propeller under hovering conditions, which is vital for drones used in Industry 4.0 applications like photogrammetry and facility inspection in automotive production. The research analyzes a straight tri-blade propeller with a NACA 0012 airfoil using analytical methods (momentum and blade element theories) and numerical simulations (ANSYS CFX with RANS method). The analytical model predicts a thrust of 1.2519 N, which is validated by simulation results showing a thrust of 1.3604 N, with an 8.67% difference, confirming the model's accuracy. These findings shows the particality of optimizing small drone propellers using combined analytical and numerical approaches. The study contributes to advancing drone designs for real-time, flexible production processes and digital twin creation in the automotive industry.
dc.description.courseMechanical Engineeringen
dc.description.degreeBSc/BA
dc.format.extent83
dc.identifier.urihttps://hdl.handle.net/2437/386702
dc.language.isoen
dc.rights.accessHozzáférhető a 2022 decemberi felsőoktatási törvénymódosítás értelmében.
dc.subjectDrone Propeller
dc.subjectSimple Momentum Theory
dc.subjectBlade Element Method
dc.subjectAnsys CFX
dc.subjectRANS
dc.subjectPropeller Forces Calculations
dc.subject.dspaceEngineering Sciences::Engineering
dc.titlePerformance Analysis of a Drone Propeller by Analytical and Numerical Methods
dc.title.translatedDrón propeller teljesítményelemzése analitikai és numerikus módszerekkel
Fájlok
Eredeti köteg (ORIGINAL bundle)
Megjelenítve 1 - 1 (Összesen 1)
Nincs kép
Név:
Performance Analysis of a Drone Propeller by Analytical and Numerical Methods.pdf
Méret:
4.02 MB
Formátum:
Adobe Portable Document Format
Leírás:
A Racing Quadcopter Propeller's aerodynamic Forces are calculated using Blade Element Theory and Validated the Results Using ANSYS CFX RANS Simulation Method.
Megjelenítés
Engedélyek köteg
Megjelenítve 1 - 1 (Összesen 1)
Nincs kép
Név:
license.txt
Méret:
1.69 KB
Formátum:
Item-specific license agreed upon to submission
Leírás:
Letöltés
Gyűjtemények
Theses (Department of Mechanical Engineering)