Preliminarni dizajn repnih površina lakog zrakoplova

master's thesis

• Title (english): Preliminary Tailplane Design for Light Aircraft
• Author: Rajan Dominić
• 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: 2020-09-24, Croatia
• Scientific / art field, discipline and subdiscipline: TECHNICAL SCIENCES; Traffic and Transport Technology; Air Traffic

Abstract

U ovom radu opisan je preliminarni dizajn repnih površina malog zrakoplova Diamond DV20, koristeći osnovne zahtjeve za stabilnost i upravljivost zrakoplova certificiranih po CS 23 regulativi. Potrebne aerodinamičke i tehničke karakteristike preuzete su iz operativnog priručnika zrakoplova, izmjerene ili proračunate metodama projektne aerodinamike. Cilj rada je prikazati međusobne odnose svih veličina potrebnih za konstrukciju repa te njihov utjecaj na stabilnost i upravljivost zrakoplova tijekom eksplotacije u svim fazama leta. Definirani su kriteriji koji moraju biti zadovoljeni pri projektiranju horizontalnog i vertikalnog stabilizatora, te je napravljen proračun repnih karakteristika za zrakoplov Diamond DV20. Na kraju rada su rezultati svih proračunatih veličina uspoređeni sa stvarnim karakteristikama repnih površina zrakoplova Katana DV20.

Abstract (english)

This paper describes the preliminary design of the tail surfaces for the small Diamond DV20 aircraft, using the basic requirements for stability and control of aircraft certified according to CS 23 regulations. The required aerodynamic and technical characteristics are taken from the aircraft operations manual, measured or calculated by aerodynamic engineering methods. The aim of this paper is to is to describe relation between main charachteristics required for tailplane design and their influence on the stability and control of aircraft during all phases of flight. The criteria that must be met when designing the horizontal and vertical stabilizer have been defined, and a calculation of the tailplane characteristics for Diamond DV20 aircraft has been made. At the end of the paper, the results of all calculated measures were compared with the actual characteristics of Katana DV20 aircraft tailplain surfaces.

• Keywords: Diamond DV20; preliminarni dizajn repnih površina; vertikalni i horizontalni stabilizator
• Keywords (english): Diamond DV 20; preliminary tailplane design; horizontal and vertical stabilizer
• Language: croatian
• URN:NBN: urn:nbn:hr:119:501202
• 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: 2020-11-17 10:06:44