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Title:
Eksperimentalna analiza osamljenega krila v zračnem toku
Authors:
ID
Rotovnik, Simon
(Author)
ID
Hribernik, Aleš
(Mentor)
More about this mentor...
ID
Bombek, Gorazd
(Comentor)
Files:
VS_Rotovnik_Simon_2013.pdf
(2,36 MB)
MD5: 2299CFF59663F65874253B1F247B647B
Language:
Slovenian
Work type:
Bachelor thesis/paper
Typology:
2.11 - Undergraduate Thesis
Organization:
FS - Faculty of Mechanical Engineering
Abstract:
V diplomskem delu smo obravnavali problematiko obtekanja osamljenega krila v zračnem toku. Pri eksperimentalni analizi smo uporabili vetrovnik, kjer smo izvedli meritve statičnega tlaka na površini osamljenega krila pri različnih napadnih kotih. Iz izmerjenih podatkov smo določili sili upora in vzgona, pri čemer nas je zanimala odvisnost koeficienta vzgona in upora od napadnega kota. Izmerjene in izračunane vrednosti smo predstavili v izrisanih grafih, jih komentirali in jih med seboj primerjali.
Keywords:
aksialni ventilator
,
osamljeno krilo
,
vetrovnik
,
eksperimentalna analiza
,
obtekanje
,
napadni kot
Place of publishing:
Maribor
Publisher:
[S. Rotovnik]
Year of publishing:
2013
PID:
20.500.12556/DKUM-42559
UDC:
533.6.07:621.63(043.2)
COBISS.SI-ID:
17595414
NUK URN:
URN:SI:UM:DK:GIVN5CSO
Publication date in DKUM:
12.11.2013
Views:
1685
Downloads:
133
Metadata:
Categories:
KTFMB - FS
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:
ROTOVNIK, Simon, 2013,
Eksperimentalna analiza osamljenega krila v zračnem toku
[online]. Bachelor’s thesis. Maribor : S. Rotovnik. [Accessed 15 March 2025]. Retrieved from: https://dk.um.si/IzpisGradiva.php?lang=eng&id=42559
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Secondary language
Language:
English
Title:
Experimental analysis of an airfoil in a free stream
Abstract:
In the thesis we discussed the issue airflow around the airfoil in the airflow. In the experimental analysis we used a wind tunnel, where we carried out measures of the static pressure on the surface of the isolated airfoil at different angles of attack. Based on the gained data we determined the friction and buoyant force, where we were interested in the dependence of the friction and buoyant coefficients on the angle of attack. The measured and calculated values are graphically presented, commented and compared among each other.
Keywords:
axial fan
,
isolated airfoil
,
wind tunnel
,
experimental analysis
,
circulation
,
angle of attack.
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