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master's thesis
PROCJENA AERODINAMIČKIH KOEFICIJENATA MODELA DRONA
Slavonski Brod: Josip Juraj Strossmayer University of Osijek, Mechanical Engineering Faculty in Slavonski Brod, 2016. urn:nbn:hr:153:418492
Knežević, Ivica
Josip Juraj Strossmayer University of Osijek
Mechanical Engineering Faculty in Slavonski Brod

Institutional repository: Repository of Mechanical Engineering in Slavonski Brod

Cite this document

Knežević, I. (2016). PROCJENA AERODINAMIČKIH KOEFICIJENATA MODELA DRONA (Master's thesis). Slavonski Brod: Josip Juraj Strossmayer University of Osijek, Mechanical Engineering Faculty in Slavonski Brod. Retrieved from https://urn.nsk.hr/urn:nbn:hr:153:418492

Knežević, Ivica. "PROCJENA AERODINAMIČKIH KOEFICIJENATA MODELA DRONA." Master's thesis, Josip Juraj Strossmayer University of Osijek, Mechanical Engineering Faculty in Slavonski Brod, 2016. https://urn.nsk.hr/urn:nbn:hr:153:418492

Knežević, Ivica. "PROCJENA AERODINAMIČKIH KOEFICIJENATA MODELA DRONA." Master's thesis, Josip Juraj Strossmayer University of Osijek, Mechanical Engineering Faculty in Slavonski Brod, 2016. https://urn.nsk.hr/urn:nbn:hr:153:418492

Knežević, I. (2016). 'PROCJENA AERODINAMIČKIH KOEFICIJENATA MODELA DRONA', Master's thesis, Josip Juraj Strossmayer University of Osijek, Mechanical Engineering Faculty in Slavonski Brod, accessed 26 December 2024, https://urn.nsk.hr/urn:nbn:hr:153:418492

Knežević I. PROCJENA AERODINAMIČKIH KOEFICIJENATA MODELA DRONA [Master's thesis]. Slavonski Brod: Josip Juraj Strossmayer University of Osijek, Mechanical Engineering Faculty in Slavonski Brod; 2016 [cited 2024 December 26] Available at: https://urn.nsk.hr/urn:nbn:hr:153:418492

I. Knežević, "PROCJENA AERODINAMIČKIH KOEFICIJENATA MODELA DRONA", Master's thesis, Josip Juraj Strossmayer University of Osijek, Mechanical Engineering Faculty in Slavonski Brod, Slavonski Brod, 2016. Available at: https://urn.nsk.hr/urn:nbn:hr:153:418492

Metadata
TitlePROCJENA AERODINAMIČKIH KOEFICIJENATA MODELA DRONA
Title (english)ASSESSMENT OF THE AERODYNAMIC COEFFICIENTS ON THE MODEL OF THE DRON
AuthorIvica Knežević
MentorDražan Kozak (mentor)
Committee memberDražan Kozak (član povjerenstva)
Committee memberŽeljko Ivandić (predsjednik povjerenstva)
Committee memberPejo Konjatić (član povjerenstva)
GranterJosip Juraj Strossmayer University of Osijek
Mechanical Engineering Faculty in Slavonski Brod
Slavonski Brod
Defense date and country2016-09-22, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Mechanical Engineering
Abstract
Cilj diplomskog rada je analiza propelera male bespilotne letjelice (drona) u vertikalnom letu i lebdenju. U prvom dijelu rada predstavljene su bespilotne letjelice, njihova primjena, te zakonska regulativa. Nakon osnovnih spoznaja o bespilotnim letjelicama i njihovoj primjeni, slijedi konfiguracija četverorotnog helikoptera. U navedenom poglavlju odabrani su i opisani dijelovi bespilotne letjelice koja je promatrana u radu. Kao pomoć pri odabiru pogonske grupe korišten je program Drive Calculator. Unutar ovog poglavlja analizirane su karakteristike aeroprofila odabranog propelera uz pomoć programa xFlr5. Nadalje, sljedećim poglavljem definiran je 3D model drona, uz određena pojednostavljenja i pretpostavke jer nisu poznati svi parametri potrebni za izradu. Model bespilotne letjelice izrađen je u programskom paketu SolidWorks 2012, gdje je definiran i materijal od kojeg je letjelica izrađena. U daljnjem radu, razmatrana je aerodinamika odabranog propelera pomoću kombinirane metode teorije diska i teorije elementarnog kraka (BEMT). U analizu su implementirani i gubitci na vrhovima krakova propelera prema Prandtlovom modelu. Naposljetku, opisano je upravljanje četverorotnim helikopterom, kao i komunikacija letjelice i operatera. Također, ukratko je opisan i način ostvarivanja stabilnosti u letu. Ovaj rad može koristiti u daljnjoj analizi horizontalnog leta, te analizi upravljivosti i stabilnosti ovog tipa letjelice.
Abstract (english)
The aim of this thesis is to analyze the propeller of small unmanned aircraft (drone) in vertical flight and hover. The first part presents the unmanned aircrafts, their use and legal regulations. After basic knowledge of unmanned aircrafts and their use, followed configuration of quadcopter. In this chapter is selected and described parts of drones which are observed in the work. To help in this selection of powertrain was used program Drive Calculator. In this chapter was analyzed the characteristics of the selected airfoil with the help of the program xFlr5. In the next chapter was defined 3D model of drone, with certain simplifications and assumptions because all parameters are not known. 3D model of unmanned aerial vehicle was made in the software package SolidWorks 2012, where is defined the material. In further work, was analyzed aerodynamics of the propeller using the Blade Element Momentum Theory (BEMT). In the analysis was implemented and losses on the tips of the propeller blades by the Prandtl model. Finally, in the next chapter was explained how to control a quadcopter, as well as communication of aircraft and operators. Also, briefly was described the way to achieve stability in flight. This work can be used in the further analysis of horizontal flight, as well as analysis of manageability and stability of this type of aircraft.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:153:418492
Study programmeTitle: Graduate Study Mechanical Engineering; specializations in: Design and Product Development, Manufacturing Logistics, Materials Engineering, Engineering Technologies, Power Engineering
Course: Design and Product Development
Study programme type: university
Study level: graduate
Academic / professional title: magistar/magistra inženjer/inženjerka strojarstva (magistar/magistra inženjer/inženjerka strojarstva)
Type of resourceText
File originBorn digital
Access conditionsAccess restricted to students and staff of home institution
Terms of useLicence In copyright icon
Created on2016-09-27 08:25:16