undergraduate thesis
Comparison of Different Airplane Cruise Regimes

Magdalena Šutej (2016)
University of Zagreb
Faculty of Transport and Traffic Sciences
Division of Aeronautics
Department of Aeronautics
Metadata
TitleUsporedba različitih režima krstarenja aviona
AuthorMagdalena Šutej
Mentor(s)Davor Franjković (thesis advisor)
Abstract
Krstarenje je segment leta aviona koji traje od trenutka kad zrakoplov nakon penjanja dostigne željenu visinu leta do trenutka kad započne spuštanje do odredišnog aerodroma. Najbitnije veličine koje se promatraju tijekom krstarenja su brzina i visina leta, dolet i specifični dolet zrakoplova. Na krstarenje velik utjecaj imaju masa aviona, koeficijent uzgona te meteorološki uvjeti. Ovisno o odnosima navedenih veličina, mogu se odrediti različiti režimi krstarenja. Izvanredne situacije koje se mogu dogoditi tijekom krstarenja također moraju biti razmotrene prilikom planiranja leta kako bi se osigurala sigurnost putnika i zrakoplova. Na primjeru aviona Airbus A320-214 analizirani su: standardno i krstarenje dugog doleta, maksimalne visine tog aviona ovisno o različitim faktorima te procedure u slučaju otkaza motora tijekom krstarenja.
Keywordsairplane cruise cruise regimes range Airbus A320-214
Parallel title (English)Comparison of Different Airplane Cruise Regimes
Committee MembersDavor Franjković (committee chairperson)
Doris Novak (committee member)
Karolina Krajček Nikolić (committee member)
Anita Domitrović (committee member)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
Lower level organizational unitsDivision of Aeronautics
Department of Aeronautics
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)
Cruise is a segment of flight from reaching the desired altitude after climb to start of a descent to land. The most important measures observed during the cruise are: velocity, altitude, range and specific range of an aircraft. Cruise is affected by airplane mass, lift coefficient and meteorological conditions. Different cruise regimes can be determined by combining different values of these factors. Emergency situations should be taken into account during flight planning to ensure safety of passengers and the aircraft. Standard cruise, long range cruise, maximum altitudes in terms of different factors and procedures in case of an engine failure have been analyzed for Airbus A320-214.
Parallel keywords (Croatian)krstarenje aviona režimi krstarenja aviona dolet aviona Airbus A320-214
Resource typetext
Access conditionOpen access
Terms of usehttp://rightsstatements.org/vocab/InC/1.0/
URN:NBNhttps://urn.nsk.hr/urn:nbn:hr:119:836920
CommitterMojca Brenko-Puzak