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undergraduate thesis
Analiza performansi zrakoplova u penjanju primjenom metode ukupne energije
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2019. urn:nbn:hr:235:188191
Vidović, Ivan
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

Vidović, I. (2019). Analiza performansi zrakoplova u penjanju primjenom metode ukupne energije (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:188191

Vidović, Ivan. "Analiza performansi zrakoplova u penjanju primjenom metode ukupne energije." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2019. https://urn.nsk.hr/urn:nbn:hr:235:188191

Vidović, Ivan. "Analiza performansi zrakoplova u penjanju primjenom metode ukupne energije." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2019. https://urn.nsk.hr/urn:nbn:hr:235:188191

Vidović, I. (2019). 'Analiza performansi zrakoplova u penjanju primjenom metode ukupne energije', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 26 December 2024, https://urn.nsk.hr/urn:nbn:hr:235:188191

Vidović I. Analiza performansi zrakoplova u penjanju primjenom metode ukupne energije [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2019 [cited 2024 December 26] Available at: https://urn.nsk.hr/urn:nbn:hr:235:188191

I. Vidović, "Analiza performansi zrakoplova u penjanju primjenom metode ukupne energije", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2019. Available at: https://urn.nsk.hr/urn:nbn:hr:235:188191

Metadata
TitleAnaliza performansi zrakoplova u penjanju primjenom metode ukupne energije
Title (english)Analysis of Aircraft Performance in Climb With Application of Total Energy Method
AuthorIvan Vidović
MentorMilan Vrdoljak (mentor)
Committee memberMilan Vrdoljak (predsjednik povjerenstva)
Committee memberIvica Smojver (član povjerenstva)
Committee memberJosip Stepanić (član povjerenstva)
Committee memberDarko Ivančević (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2019-03-01, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
Tema ovog završnog rada je analiza i usporedba performansi zrakoplova u penjanju primjenom metode ukupne energije. Promatrat će se zrakoplovi koji prema karakteristikama nalikuju MiG-21bis i F-16 Block52. Na početku su izračunate sve karakteristike otpora za MiG-21 sa raketama i bez njih, kao i za F-16 sa raketama. Nakon čega se računaju karakteristike pogona. Pomoću sile pogona i otpora prikazana su područja mogućeg leta na različitim visinama, u kojima pogonska sila nadjačava otpor. Koristeći navedene sile izračunava se višak snage, kao bitan faktor određivanja vremena trajanja leta. Zrakoplovi se promatraju kao središte mase koje ima sve izračunate karakteristike. Primjenom metode ukupne energije određuju se režimi koji daju minimalno vrijeme trajanja leta. Na temelju dobivenih rezultata, uspoređuju se zrakoplovi i analizira se prednost jednoga u odnosu na drugi i obrnuto.
Abstract (english)
Topic of this bachelor thesis is analysis and comparison of the aircraft performances while climbing, using the minimal energy method. Examined aircraft's characteristics resemble the MiG-21bis and F-16 Block52. At the beginning all the characteristics of the drag are calculated both for the MiG-21 with two missiles and without them, like the ones for the F-16 with two missiles. Thrust characteristics are calculated after it. Using the results of the drag and the thrust, region where flight can be sustained is shown, that is the area where thrust overcomes the drag. Using the given forces excess power is calculated, which is a essential for calculating time of the flight. Aircraft are examined like a mass point which have all the characteristics as calculated. Minimal flight time regimes are determined using the minimal energy method. Using the results, aircraft are compared and advantage of one over another is analysed.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:188191
Study programmeTitle: Aeronautical Studies
Study programme type: university
Study level: undergraduate
Academic / professional title: sveučilišni/a prvostupnik/ prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka zrakoplovnog inženjerstva (sveučilišni/a prvostupnik/ prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka zrakoplovnog inženjerstva)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2019-05-28 09:49:01