prikaz prve stranice dokumenta Model leta helikoptera temeljen na modelu gibanja materijalne točke
  Download
PDF 3.06 MB
master's thesis
Model leta helikoptera temeljen na modelu gibanja materijalne točke
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. urn:nbn:hr:235:008628
Bračić, Roko
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

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

Cite this document

Bračić, R. (2024). Model leta helikoptera temeljen na modelu gibanja materijalne točke (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:008628

Bračić, Roko. "Model leta helikoptera temeljen na modelu gibanja materijalne točke." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. https://urn.nsk.hr/urn:nbn:hr:235:008628

Bračić, Roko. "Model leta helikoptera temeljen na modelu gibanja materijalne točke." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. https://urn.nsk.hr/urn:nbn:hr:235:008628

Bračić, R. (2024). 'Model leta helikoptera temeljen na modelu gibanja materijalne točke', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 28 December 2024, https://urn.nsk.hr/urn:nbn:hr:235:008628

Bračić R. Model leta helikoptera temeljen na modelu gibanja materijalne točke [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2024 [cited 2024 December 28] Available at: https://urn.nsk.hr/urn:nbn:hr:235:008628

R. Bračić, "Model leta helikoptera temeljen na modelu gibanja materijalne točke", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2024. Available at: https://urn.nsk.hr/urn:nbn:hr:235:008628

Metadata
TitleModel leta helikoptera temeljen na modelu gibanja materijalne točke
Title (english)Helicopter flight model based on point mass model
AuthorRoko Bračić
MentorMilan Vrdoljak (mentor)
MentorMarijan Andrić (komentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2024-12-06, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
U diplomskom radu prikazan je postupak izrade i implementacija modela leta temeljenog na modelu gibanja materijalne točke. Prikazane su sve potrebne geometrijske i aerodinamičke karakteristike razmatranog helikoptera Bo105, te su opisana dva različita načina proračuna ravnotežnog leta helikoptera. Prvi proračun izvršen je prema Van Hoydonck-u, te je za njega potrebno manje računalnih resursa od drugog proračuna prema Bramwell-u, koji pruža kompletniju i precizniju sliku parametara ravnotežnog leta. Nadalje, proračun prema Bramwell-u dodatno prikazuje i rezultate za bočnu ravnotežu. Opisan je postupak implementacije parametara ravnotežnog leta u model leta te je prikazana izrada dva modela leta različite kompleksnosti. Za oba modela su provedene demonstracije složene trajektorije za koje su prikazani rezultati.
Abstract (english)
Main topic of this master's thesis is the process of creation and implementation of a helicopter flight model based on point mass model. Helicopter used as example in the thesis is Bo105, whose aerodynamic and geometric parameters were shown, as well as two different approaches to calculation of the helicopter trim conditions. First approach to trim was done according to Van Hoydonck, which was less complex and thus faster than the second approach, which was done according to Bramwell. However, Bramwell's approach turned to be more precise and complete. Also, it included calculation of lateral trim. Implementation of trim conditions to the model were described, and two models of different complexity were created and explained. In the end, both models have been tested and the results of flight parameters were shown and analysed.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:008628
Study programmeTitle: Aeronautical Engineering
Study programme type: university
Study level: graduate
Academic / professional title: sveučilišni/a magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva (sveučilišni/a magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2024-12-03 14:28:47