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master's thesis
Aerotermodinamički problemi zrakoplovnih konstrukcija
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2009. urn:nbn:hr:235:064831
Perak, Agata
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

Cite this document

Perak, A. (2009). Aerotermodinamički problemi zrakoplovnih konstrukcija (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:064831

Perak, Agata. "Aerotermodinamički problemi zrakoplovnih konstrukcija." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2009. https://urn.nsk.hr/urn:nbn:hr:235:064831

Perak, Agata. "Aerotermodinamički problemi zrakoplovnih konstrukcija." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2009. https://urn.nsk.hr/urn:nbn:hr:235:064831

Perak, A. (2009). 'Aerotermodinamički problemi zrakoplovnih konstrukcija', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 19 April 2024, https://urn.nsk.hr/urn:nbn:hr:235:064831

Perak A. Aerotermodinamički problemi zrakoplovnih konstrukcija [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2009 [cited 2024 April 19] Available at: https://urn.nsk.hr/urn:nbn:hr:235:064831

A. Perak, "Aerotermodinamički problemi zrakoplovnih konstrukcija", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2009. Available at: https://urn.nsk.hr/urn:nbn:hr:235:064831

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Metadata
TitleAerotermodinamički problemi zrakoplovnih konstrukcija
AuthorAgata Perak
MentorIvanka Boras (mentor)
MentorIvica Smojver (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2009-11-19, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
Cilj ovog rada bio je opisati teorijske osnove aerotermodinamike i navesti aerotermodinamičke probleme zrakoplovnih konstrukcija. Definirano je hiperzvučno strujanje i navedene su klase hiperzvučnih letjelica. Pojave i problemi koji se javljaju pri tako velikim toplinskim opterećenjima analizirane su za slučaj Space Shuttle-a , kao jedine operativne hiperzvučne letjelice. Napravljen je proračun radijacijske-adijabatske temperature stijenke kao dobre procjene stvarne temperature površine letjelice. Izvršena je parametarska analiza te usporedba sa podacima iz literature.
Keywords
Languagecroatian
URN:NBNurn:nbn:hr:235:064831
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
RepositoryRepository of Faculty of Mechanical Engineering and Naval Architecture University of Zagreb
Created on2019-05-27 12:46:03

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