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master's thesis
Eksperimentalno određivanje karakteristika aerodinamičke buke na modelu aeroprofila
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2018. urn:nbn:hr:119:140110
Fujs, David
University of Zagreb
Faculty of Transport and Traffic Sciences
Division of Aeronautics
Department of Aeronautics

Institutional repository: Faculty of Transport and Traffic Sciences

Cite this document

Fujs, D. (2018). Eksperimentalno određivanje karakteristika aerodinamičke buke na modelu aeroprofila (Master's thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:140110

Fujs, David. "Eksperimentalno određivanje karakteristika aerodinamičke buke na modelu aeroprofila." Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2018. https://urn.nsk.hr/urn:nbn:hr:119:140110

Fujs, David. "Eksperimentalno određivanje karakteristika aerodinamičke buke na modelu aeroprofila." Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2018. https://urn.nsk.hr/urn:nbn:hr:119:140110

Fujs, D. (2018). 'Eksperimentalno određivanje karakteristika aerodinamičke buke na modelu aeroprofila', Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 29 December 2024, https://urn.nsk.hr/urn:nbn:hr:119:140110

Fujs D. Eksperimentalno određivanje karakteristika aerodinamičke buke na modelu aeroprofila [Master's thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2018 [cited 2024 December 29] Available at: https://urn.nsk.hr/urn:nbn:hr:119:140110

D. Fujs, "Eksperimentalno određivanje karakteristika aerodinamičke buke na modelu aeroprofila", Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2018. Available at: https://urn.nsk.hr/urn:nbn:hr:119:140110

Metadata
TitleEksperimentalno određivanje karakteristika aerodinamičke buke na modelu aeroprofila
Title (english)Experimental Assessment of Aerodynamic Noise Characteristics on an Airfoil Model
AuthorDavid Fujs
MentorTino Bucak (mentor)
Committee memberAnita Domitrović (predsjednik povjerenstva)
Committee memberJurica Ivošević (član povjerenstva)
Committee memberDoris Novak (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2018-05-08, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Mjerenja zrakoplovne buke imaju sve značajniju ulogu u zrakoplovnoj industriji. Postoji više metoda mjerenja i analize za različite potrebe i vrste zrakoplovne buke. Najjednostavniji mjerni senzor je piezoelektrični pretvarač koji radi svojih reverzibilnih svojstava može imati ulogu mikrofona. Pri mjerenju aerodinamičke buke na aeroprofilu on je odličan izbor radi svojih malih dimenzija. Za određivanje karakteristika aerodinamičke buke potrebno je kondicijsko pojačalo za pojačanje izmjerenog signala na senzoru, stoga se ono izrađuje. Za potrebe mjerenja također se dizajnira i izrađuje model aeroprofila NACA 2421 s ugrađenim mjernim senzorima. Ugradnjom aeroprofila u aerotunel i spajanjem senzora na računalo preko pojačala, moguće je izmjeriti buku, obraditi podatke i analizirati dobivene rezultate. Korištenjem određenih korekcija moguće je poboljšanje u prikazu rezultata i ispravljanje za neke greške u mjerenjima. U diskusiji su doneseni zaključci o mjerenjima i uočene neke korelacije. Primijenjena metoda se pokazuje vrlo uspješnom i prigodnom za ovakav eksperiment. Također, mogućnosti daljnjeg razvoja i unaprjeđenja metode su mnogobrojne.
Abstract (english)
The role of aircraft noise measurements is becoming more significant for aircraft industry. Various methods of measurement and analysis exist for different uses and types of aircraft noise. The simplest measuring sensor is piezoelectric transducer which can be used as a microphone due to its reversal characteristics. Small dimensions make it a good choice for measurements of aerodynamic noise on an airfoil. Condition amplifier is needed for amplification of signals detected by sensors and for assessment of aerodynamic noise, therefore it is being constructed as well. An airfoil model NACA 2421 with piezoelectric sensors is being designed for the experiment. The airfoil is assembled in wind tunnel which allows noise measurement, data processing and result analysis to be made. By using some measurement correction methods it is possible to improve data representation. Conclusions about measurements and observed correlations are discussed and reviewed. This particular applied method is shown to be very efficient and practical for this kind of experiment. Moreover, there is a lot of potential for improving the method and further development.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:140110
Study programmeTitle: Aeronautics
Study programme type: university
Study level: graduate
Academic / professional title: magistar/magistra inženjer/inženjerka aeronautike (magistar/magistra inženjer/inženjerka aeronautike)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2018-05-15 16:38:45