undergraduate thesis
Simulation of Obstruction in Static Pressure Inlet

Marko Pejković (2016)
Sveučilište u Zagrebu
Fakultet prometnih znanosti
Aeronautika
Zavod za aeronautiku
Metadata
TitleSimulacija začepljenja otvora statičkog tlaka zrakoplova
AuthorMarko Pejković
Mentor(s)Jurica Ivošević (thesis advisor)
Abstract
Simulacija prikaza začepljenja otvora statičkog tlaka zrakoplova izrađena je u programskom okruženju Matlab Simulink. Pomoću blokova i dijagrama toka ostvaren je algoritam te su rezultati korišteni za simulaciju. Objašnjeni su odnosi među tlakovima zraka, te sustavi statičkog i ukupnog tlaka zraka. Analizirana je brzina leta te instrumeni koji mjere i prikazuju brzinu leta, isto tako i visina leta sa odgovarajućim instrumentima. Prikazane su greške začepljenja otvora statičkog tlaka zraka u penjanju i spuštanju zrakoplova te su prikazane u simulaciji.
Keywordssimulation of occlusion static port of aircraft MatlabSimulink air pressure indication of flight speed indication of altitude of flight
Parallel title (English)Simulation of Obstruction in Static Pressure Inlet
Committee MembersJurica Ivošević (committee chairperson)
Tino Bucak (committee member)
Davor Franjković (committee member)
Željko Marušić (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 date2016-09-13
Parallel abstract (English)
Simulation of occulsion of static port of aircraft is made in software environment MatlabSimulink. Block diagrams are used to create flowchart, which contain algorithms. The results gained from the algorithms are used in the simulations. Relations between air pressure and systems of static and total air pressure are explained in this final thesis. Flight speed and instreuments, flight altitude and instruments are analyzed too. Occlusion of static port in climb and descent are shown in simulation.
Parallel keywords (Croatian)simulacija začepljenja statički otvor zrakoplova Matlab Simulink tlak zraka indikacija brzine leta indikacija visine leta
Resource typetext
Access conditionOpen access
Terms of usehttp://rightsstatements.org/vocab/InC/1.0/
URN:NBNhttps://urn.nsk.hr/urn:nbn:hr:119:973036
CommitterMojca Brenko-Puzak