undergraduate thesis
The Design of Aircraft with Piston Engine

Tomislav Banić (2015)
Sveučilište u Zagrebu
Fakultet prometnih znanosti
Promet
Zavod za zračni promet
Metadata
TitleDizajn zrakoplova s klipnim pogonom
AuthorTomislav Banić
Mentor(s)Andrija Vidović (thesis advisor)
Abstract
U ovom završnom radu prikazan je proces dizajniranja zrakoplova te svi parametri potrebni kako bi se ostvarila uspješna konstrukcija. Kroz rad će se definirati osnove dizajniranja zrakoplovne strukture, te prikazati osnovni konstruktivni zahtjevi i podaci za konstruiranje i osnovne faze dizajniranja zrakoplova. Prikazat će se glavne točke konceptualnog dizajna zrakoplova zajedno sa svim potrebnim parametrima i analizama. U završnom radu bit će dani primjeri dizajniranja zrakoplova Flayer I i DC - 3 gdje će biti prikazani postupci analiziranja i konstruiranja te prikaz parametara prethodno navedenih zrakoplova. Kroz zaključak ovog rada bit će predočeni rezultati istraživanja i zaključna razmatranja prethodno navedenih poglavlja i specifičnosti dizajna zrakoplova s klipnim motorom.
Keywordsdesign aircraft piston engine construction phases performances
Parallel title (English)The Design of Aircraft with Piston Engine
Committee MembersAndrija Vidović
Anita Domitrović
Miroslav Borković
Sanja Steiner
GranterSveučilište u Zagrebu
Fakultet prometnih znanosti
Lower level organizational unitsPromet
Zavod za zračni promet
PlaceZagreb
StateCroatia
Scientific field, discipline, subdisciplineTECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Aircraft Construction and Design
Study programme typeuniversity
Study levelundergraduate
Study programmeRoad Transport, Railway Transport, Water Transport, Air Transport, Postal Transport, Information and Communications Traffic, Urban Transport
Academic title abbreviationuniv. bacc. ing. traff.
Genreundergraduate thesis
Language Croatian
Defense date2015-09-15
Parallel abstract (English)
In this final paper, the process of designing the aircraft and all the parameters needed to achieve a successful construction are shown. Through the work we will define the basics of designing aerospace structures, and show basic structural requirements and data for design and basic design phase of the aircraft. You will see the main points of the conceptual design of the aircraft, together with all the required parameters and analysis. In this final paper will be given examples of designing aircraft Flyer I and DC - 3 where it will be shown the procedures to analyze and construct and display parameters of the above aircraft. Through the conclusion of this work will be presented the results of studies and concluding remarks of the above sections and the specifics of the design of aircraft with piston engine.
Parallel keywords (Croatian)dizajn zrakoplov klipni pogon faze konstruiranja performanse
Resource typetext
Access conditionOpen access
Terms of usehttp://rightsstatements.org/vocab/InC/1.0/
URN:NBNhttps://urn.nsk.hr/urn:nbn:hr:119:117681
CommitterMojca Brenko-Puzak