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master's thesis
Aerodynamic model development for general aviation aircraft based on flight test data
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2021. urn:nbn:hr:235:592022
Đeverlija, Jan Juraj
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

Institutional repository: Repository of Faculty of Mechanical Engineering and Naval Architecture University of Zagreb

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Đeverlija, J. J. (2021). Aerodynamic model development for general aviation aircraft based on flight test data (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:592022

Đeverlija, Jan Juraj. "Aerodynamic model development for general aviation aircraft based on flight test data." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2021. https://urn.nsk.hr/urn:nbn:hr:235:592022

Đeverlija, Jan Juraj. "Aerodynamic model development for general aviation aircraft based on flight test data." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2021. https://urn.nsk.hr/urn:nbn:hr:235:592022

Đeverlija, J. J. (2021). 'Aerodynamic model development for general aviation aircraft based on flight test data', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 25 November 2024, https://urn.nsk.hr/urn:nbn:hr:235:592022

Đeverlija JJ. Aerodynamic model development for general aviation aircraft based on flight test data [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2021 [cited 2024 November 25] Available at: https://urn.nsk.hr/urn:nbn:hr:235:592022

J. J. Đeverlija, "Aerodynamic model development for general aviation aircraft based on flight test data", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2021. Available at: https://urn.nsk.hr/urn:nbn:hr:235:592022

Metadata
TitleAerodynamic model development for general aviation aircraft based on flight test data
Title (croatian)Razvoj aerodinamičkog modela aviona opće avijacije temeljem podataka s testnih letova
AuthorJan Juraj Đeverlija
MentorMilan Vrdoljak (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2021-12-16, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Aircraft Control
Abstract
This master thesis is a continuation of the work on a project of aerodynamic model development for a general aviation airplane, Piper PA-28, conducted by Centre for aviation at the Zürich University of Applied Sciences. After previous flight test data processing and organizing, a basic linear model was introduced. In this thesis its improvement was made, but before improvement itself, using flight path reconstruction it is necessary to develop sensor error model, as precisely as possible. Great attention is dedicated exactly to this part. Completion of the flight path reconstruction, with corrected sensor values, using linear regression aerodynamic parameters are estimated with ordinary least square method. Focus is put on longitudinal motion, such as stall, phugoid and short period manoeuvres.
Abstract (croatian)
Ovaj diplomski radi nastavak je rada na projektu razvoja aerodinamičkog modela zrakoplova generalne avijacije, Piper PA-28, Centra za zrakoplovstvo Sveučilišta primijenjenih znanosti u Zürichu. Nakon prethodne obrade i organizacije podataka snimljenih tijekom leta, predstavljen je osnovni linearni model. U ovom diplomskom radu napravljeno je poboljšanje, ali prije samog rada na poboljšavanju modela, putem rekonstrukcije putanje leta potrebno je što preciznije obraditi model pogrešaka senzora. Velika pažnja posvećena je upravo tom dijelu. Završetkom rekonstrukcije putanje lete, s korigiranim vrijednostima senzora, primjenom linearne regresije metodom najmanjih kvadrata procjenjuju se aerodinamički parametri. Fokus je stavljen na uzdužno gibanje, poput sloma uzgona, dugo periodičnog i kratko periodičnog moda.
Keywords
Keywords (croatian)
Languageenglish
URN:NBNurn:nbn:hr:235:592022
Study programmeTitle: Aeronautical Studies
Study programme type: university
Study level: graduate
Academic / professional title: magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva (magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Public noteThis thesis was done in association with Centre for Aviation at the Zürich University of Applied Sciences (ZHAW). Co-mentor from ZHAW was Dr. Pierluigi Capone.
Created on2021-12-13 23:04:06