prikaz prve stranice dokumenta Proračun induciranog otpora letu zrakoplova
  Download
PDF 2.15 MB
undergraduate thesis
Proračun induciranog otpora letu zrakoplova
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2019. urn:nbn:hr:119:459368
Glas, Luka Mihovil
University of Zagreb
Faculty of Transport and Traffic Sciences
Division of Aeronautics
Department of Aeronautics

Institutional repository: Faculty of Transport and Traffic Sciences

Cite this document

Glas, L. M. (2019). Proračun induciranog otpora letu zrakoplova (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:459368

Glas, Luka Mihovil. "Proračun induciranog otpora letu zrakoplova." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2019. https://urn.nsk.hr/urn:nbn:hr:119:459368

Glas, Luka Mihovil. "Proračun induciranog otpora letu zrakoplova." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2019. https://urn.nsk.hr/urn:nbn:hr:119:459368

Glas, L. M. (2019). 'Proračun induciranog otpora letu zrakoplova', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 05 July 2024, https://urn.nsk.hr/urn:nbn:hr:119:459368

Glas LM. Proračun induciranog otpora letu zrakoplova [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2019 [cited 2024 July 05] Available at: https://urn.nsk.hr/urn:nbn:hr:119:459368

L. M. Glas, "Proračun induciranog otpora letu zrakoplova", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2019. Available at: https://urn.nsk.hr/urn:nbn:hr:119:459368

Metadata
TitleProračun induciranog otpora letu zrakoplova
Title (english)Calculation of Airplane Induced Drag
AuthorLuka Mihovil Glas
MentorDavor Franjković (mentor)
Committee memberAnita Domitrović (predsjednik povjerenstva)
Committee memberKarolina Krajček Nikolić (član povjerenstva)
Committee memberErnest Bazijanac (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2019-09-17, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Na zrakoplov u letu djeluju četiri sile: sila uzgona, sila potiska, težina zrakoplova i sila otpora. Sila otpora sastoji se od dvije komponente, parazitnog i induciranog otpora. Inducirani otpor nastaje kao posljedica proizvodnje uzgona, većinom na krilima zrakoplova, i predstavlja značajan udio u ukupnom otporu u određenim fazama leta. Također, uz pojavu induciranog otpora nastaju i vršni vrtlozi koji mogu biti opasni za druge zrakoplove tijekom operacija u blizini aerodroma. Prilikom dizajniranja zrakoplova i proračuna performansi bitno je znati utjecaj pojedinih dijelova zrakoplova na veličinu induciranog otpora te se koriste oni dijelovi koji u najvećoj mjeri smanjuju inducirani otpor zrakoplova, tj. poboljšavaju performanse zrakoplova.
Abstract (english)
There are four forces that act on an aircraft in flight, those are: lift, thrust, weight and drag. Drag is consisted of two components: parasitic drag and induced drag. Induced drag is a byproduct of lift production, mostly on aircraft wings, and makes a major part in total drag of an aircraft in certain part of flight. Wing tip vortices are closely related to induced drag and can be very dangerous to other aircraft which are operating in the vicinity of an aerodrome. While designing an aircraft and studying its performance, it is important to know how each part of an aircraft influences induced drag, both individually and combined with other parts, so that only the best parts can be used.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:459368
Study programmeTitle: Aeronautics
Study programme type: university
Study level: undergraduate
Academic / professional title: sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike (sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2019-09-23 13:16:55