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master's thesis
Eksperimentalna Ljungströmova turbina
2012. urn:nbn:hr:235:104641
Basta, Dijana
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

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Basta, D. (2012). Eksperimentalna Ljungströmova turbina (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:104641

Basta, Dijana. "Eksperimentalna Ljungströmova turbina." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2012. https://urn.nsk.hr/urn:nbn:hr:235:104641

Basta, Dijana. "Eksperimentalna Ljungströmova turbina." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2012. https://urn.nsk.hr/urn:nbn:hr:235:104641

Basta, D. (2012). 'Eksperimentalna Ljungströmova turbina', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 14 February 2025, https://urn.nsk.hr/urn:nbn:hr:235:104641

Basta D. Eksperimentalna Ljungströmova turbina [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2012 [cited 2025 February 14] Available at: https://urn.nsk.hr/urn:nbn:hr:235:104641

D. Basta, "Eksperimentalna Ljungströmova turbina", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2012. Available at: https://urn.nsk.hr/urn:nbn:hr:235:104641

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Metadata
TitleEksperimentalna Ljungströmova turbina
Title (english)Experimental Ljungström turbine
AuthorDijana Basta
MentorZvonimir Guzović (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2012-11-23, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Mechanical Engineering
Abstract
Zadaća ovog rada je napraviti preliminarni proračun plinske turbine koja bi služila pogonu bespilotne letjelice za nadzor teritorija. U radu su prikazane podjele postojećih letjelica s opisima i naglaskom na pogone. Letjelice su svrstane u dvije glavne grupe s obzirom na razlike pogona i principa leta. To su letjelice krutih nosećih površina i letjelice tipa zračni brodovi. Po dostupnim podacima izvršen je preliminarni proračun radijalne plinske turbine i preko programskog rješenja za termodinamičke proračune REFPROP izvršen je termodinamički proračun. Kao radni fluid, u razmatranje su uzeti helij i zrak, s obzirom da oni mogu poslužiti za punjenje same letjelice. Izračun je izvršen za zrak i helij te se tako mogu vidjeti razlike u konstrukciji turbine s obzirom na radni plin.
Keywords
Languagecroatian
URN:NBNurn:nbn:hr:235:104641
Study programmeTitle: Aeronautical Studies
Study programme type: university
Study level: graduate
Academic / professional title: diplomirani inženjer/inženjerka zrakoplovstva (diplomirani inženjer/inženjerka zrakoplovstva)
Type of resourceText
File originBorn digital
Access conditionsAccess restricted to students and staff of home institution
Terms of useLicence In copyright icon
Created on2019-05-22 02:15:43