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undergraduate thesis
Izračun performansi jednomotornog zrakoplova s propelerskim pogonom
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. urn:nbn:hr:119:413384
Mandić, Domagoj
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

Mandić, D. (2017). Izračun performansi jednomotornog zrakoplova s propelerskim pogonom (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:413384

Mandić, Domagoj. "Izračun performansi jednomotornog zrakoplova s propelerskim pogonom." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. https://urn.nsk.hr/urn:nbn:hr:119:413384

Mandić, Domagoj. "Izračun performansi jednomotornog zrakoplova s propelerskim pogonom." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. https://urn.nsk.hr/urn:nbn:hr:119:413384

Mandić, D. (2017). 'Izračun performansi jednomotornog zrakoplova s propelerskim pogonom', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 29 December 2024, https://urn.nsk.hr/urn:nbn:hr:119:413384

Mandić D. Izračun performansi jednomotornog zrakoplova s propelerskim pogonom [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2017 [cited 2024 December 29] Available at: https://urn.nsk.hr/urn:nbn:hr:119:413384

D. Mandić, "Izračun performansi jednomotornog zrakoplova s propelerskim pogonom", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2017. Available at: https://urn.nsk.hr/urn:nbn:hr:119:413384

Metadata
TitleIzračun performansi jednomotornog zrakoplova s propelerskim pogonom
Title (english)Performance Calculations of Single Engine Propeller-driven Aircraft
AuthorDomagoj Mandić
MentorDavor Franjković (mentor)
Committee memberAnita Domitrović (predsjednik povjerenstva)
Committee memberTomislav Radišić (član povjerenstva)
Committee memberŽeljko Marušić (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2017-09-12, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Performanse predstavljaju specifičnu skupinu mogućnosti i sposobnosti koju određeni zrakoplov posjeduje u rasponu različitih masa i brzina na određenim visinama. Gledano sa stajališta fazi leta, specijalnim performansama se smatraju faze polijetanja, slijetanja i zaokreta zrakoplova. Kroz cjelokupni rad analizirani su osnovni elementi izračuna u pogledu fizikalnih zakona za različite faze leta (horizontalni let, penjanje, spuštanje, polijetanje, slijetanje i zaokreti), a nakon svakog režima leta, kao zasebnog poglavlja. Također, prikazani su proračunati parametri za specifične mase i visine, unutar raspona masa, zrakoplova Beechcraft Bonanza. Prikaz proračunatih parametara, ovisno o fazi leta, prikazani su kroz nekoliko grafikona i tablica. Kroz analiziranu materiju, spominju se i bitni vanjski čimbenici koji pridonose cjelokupnom izračunu performansi, kao i karakteristike zrakoplova poput mase, pogonske grupe, konstruktivnih te aerodinamičkih karakteristika.
Abstract (english)
Performance represent the specific group of capabilities and abilities which some aircraft possess in different span of masses and velocities values at certain altitudes. Viewed from the standpoint of the flight phases: take off, landing and an airplane turn are considered as the special performance. Throughout work, the calculations regarding physical laws for the different flight phases (level flight, climbing, descending, take off, landing and turns), are analyzed as the separate chapter. The calculated parameters of Beechcraft Bonanza, for the different span of masses and altitudes within defined range are shown as well. The calculated parameters review, depending on flight phases, are shown through several charts and tables. Throughout analyzed matter, major external factors are mentioned, which contribute overall performance calculation as well as an aircraft characteristics like mass, powerplant, construction and aerodynamics.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:413384
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 on2017-09-19 10:07:02