| dc.contributor.author | Shuvo, Dewan Emran Mahamud | |
| dc.date.accessioned | 2025-07-07T10:03:25Z | |
| dc.date.available | 2025-07-07T10:03:25Z | |
| dc.date.issued | 2025-05-19 | |
| dc.identifier.uri | http://suspace.su.edu.bd/handle/123456789/1726 | |
| dc.description.abstract | The wind tunnel is a tool used in aerodynamic research to study the effects of wind moving over
a solid object. This thesis work is done to performance test of a low-subsonic wind tunnel by
our Sonargaon university lab. We get Mach number 0.02 and the Reynolds Number is 53578
for a designed test airfoil of 150 mm for a test section of 910 mm of length. With the target of
having a flow speed about 7.02 m/s at the test section of 0.32 m2 cross-sectional area all the
other sections of the wind tunnel have been designed and using a sixth-order polynomial
equation. The wind tunnel operates at speeds below Mach 0.3 and using Java foil software for
calculation. | en_US |
| dc.language.iso | en_US | en_US |
| dc.publisher | Sonargaon University (SU) | en_US |
| dc.relation.ispartofseries | ;BME-251083 | |
| dc.subject | Low-Subsonic Wind Tunnel Present at SU Campus | en_US |
| dc.title | Performance Test of the Low-Subsonic Wind Tunnel Present at SU Campus | en_US |
| dc.type | Thesis | en_US |
