undergraduate thesis
Mathematical Model of Turboprop Engine for Determing Aircraft Performance in Steady Flight

Juraj Đurinović (2016)
Sveučilište u Zagrebu
Fakultet prometnih znanosti
Aeronautika
Zavod za aeronautiku
Metadata
TitleMatematički model elisno - mlaznog motora za određivanje performansi zrakoplova u ravnotežnom letu
AuthorJuraj Đurinović
Mentor(s)Anita Domitrović (thesis advisor)
Abstract
U ovom završnom radu dan je matematički model elisno-mlaznog motora koji može poslužiti za izračun snage motora u ravnotežnom letu zrakoplova. Općenito se opisuje konstrukcija mlaznih, odnosno elisno-mlaznih motora i dodatno se iznose karakteristike na primjeru motora ugrađenog na zrakoplov DASH 8 Q 400, odnosno motora P&W150A. Objašnjava se horizontalni let zrakoplova i postavljaju se uvjeti ravnoteže. Definiran je matematički model motora i prikazani su dijagrami koji prikazuju ovisnost potiska, snage, specifične potrošnje goriva i masenog protoka zraka o brzini zrakoplova, odnosno Machovom broju.
Keywordsturboprop engine engine performance steady aircraft flight
Parallel title (English)Mathematical Model of Turboprop Engine for Determing Aircraft Performance in Steady Flight
Committee MembersAnita Domitrović (committee chairperson)
Ernest Bazijanac (committee member)
Karolina Krajček Nikolić (committee member)
Doris Novak (committee member)
GranterSveučilište u Zagrebu
Fakultet prometnih znanosti
Lower level organizational unitsAeronautika
Zavod za aeronautiku
PlaceZagreb
StateCroatia
Scientific field, discipline, subdisciplineTECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Study programme typeuniversity
Study levelundergraduate
Study programmeAeronautics
Academic title abbreviationuniv. bacc. ing. aeronaut.
Genreundergraduate thesis
Language Croatian
Defense date2016-07-05
Parallel abstract (English)
This thesis analyses mathematical model of turboprop engine which can be used for calculating power of engine in aircraft steady flight. Construction of turboprop engine is described in general and also on example of DASH 8 Q 400's engine, P&W150A. Steady flight of aircraft is explained and balance terms are derived. Mathematical model of turboprop engine is developed and figures of variation of thrust, power, specific fuel consumption and mass flow are shown dependent on aircraft speed - Mach number.
Parallel keywords (Croatian)elisno-mlazni motor performanse motora ravnotežni let zrakoplova
Resource typetext
Access conditionOpen access
Terms of usehttp://rightsstatements.org/vocab/InC/1.0/
URN:NBNhttps://urn.nsk.hr/urn:nbn:hr:119:178792
CommitterMojca Brenko-Puzak