Konceptualni dizajn i performanse bespilotne letjelice s kanardima

master's thesis

• Title (english): Conceptual Design and Performance Evaluation of Unmanned Aerial Vehicle with Canard Configuration
• Author: Nikola Renčelj
• Mentor: Karolina Krajček Nikolić (mentor)
• Committee member: Anita Domitrović (predsjednik povjerenstva)
• Committee member: Davor Franjković (član povjerenstva)
• Committee member: Ernest Bazijanac (član povjerenstva)
• Granter: University of Zagreb; Faculty of Transport and Traffic Sciences; (Division of Aeronautics); (Department of Aeronautics); Zagreb
• Defense date and country: 2017-09-26, Croatia
• Scientific / art field, discipline and subdiscipline: TECHNICAL SCIENCES; Traffic and Transport Technology; Air Traffic

Abstract

U ovom diplomskom radu izvršena je analiza konceptualnog dizajna letjelice koju su osmislili i konstruirali studenti studija aeronautike. Opisan je i objašnjen proces dimenzioniranja uzgonskih površina, uzročno-posljedični odnos izmjene geometrije uzgonskih površina i specifičnosti odabrane konfiguracije. Određene su i osnovne performanse putem proračuna otpora metodama projektne aerodinamike i uz pomoć aproksimacije performansi pogonske grupe. Objašnjene su metode testiranja kako bi se osigurala sposobnost zrakoplova za let u stvarnim uvjetima.

Abstract (english)

This thesis summarizes the development process of an unmanned aerial vehicle, which was designed and built by students of the Aeronautics department. Specifically, it elaborates the process of sizing the lifting surfaces, effects of geometry changes and specific requirements of the chosen configuration. Basic performance figures were estimated through drag and propulsion approximations. Lastly, testing methods with the purpose of verifying stability calculations and safely getting the aircraft airborne were described.

• Keywords: uzgonske površine; kanardi; bespilotna letjelica; performanse; ispitivanje; neutralna točka; stabilnost; XFLR5; OpenVSP
• Keywords (english): lifting surfaces; canard; unmanned aerial vehicle; UAV; performance; testing; neutral point; stability; XFLR5; OpenVSP
• Language: croatian
• URN:NBN: urn:nbn:hr:119:002589
• Study programme: Title: Aeronautics; Study programme type: university; Study level: graduate; Academic / professional title: magistar/magistra inženjer/inženjerka aeronautike (magistar/magistra inženjer/inženjerka aeronautike)
• Type of resource: Text
• File origin: Born digital
• Access conditions: Open access
• Created on: 2017-10-05 12:06:44