| 000 | 01905nam a2200253 a 4500 | ||
|---|---|---|---|
| 001 | vtls000066760 | ||
| 003 | KUKTEM | ||
| 005 | 20251114204531.0 | ||
| 008 | 121122t2012 my da f m 000 0 eng d | ||
| 020 | _aTHE0007589(Local) | ||
| 039 | 9 |
_a201905171116 _bfawwaz _c201211291120 _dhuda _c201211291119 _dhuda _c201211271504 _dhuda _y201211221014 _zhuda |
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| 040 | _aUMP | ||
| 090 | _aTS171.4 .K66 2012 rs Bc. | ||
| 100 | 1 | _aKoo, Nelton Chwee Yang | |
| 245 | 1 | 0 |
_aDesign of wind tunnel (fluid flow analysis) / _cNelton Koo Chwee Yang |
| 260 |
_aKuantan, Pahang : _bUMP, _c2012 |
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| 300 |
_axvii, 53 p. : _bill. (some col.) ; _c30 cm. + _e1 CD-ROM |
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| 502 | _aProject paper (Bachelor of Manufacturing Engineering) -- Universiti Malaysia Pahang - 2012 | ||
| 504 | _aBibliography : p. 47-48 | ||
| 520 | 3 | _aA low speed wind tunnel was design and fabricate. The project covered the process of design and fabrication of the small wind tunnel. In completing this project, a computer aided drawing (CAD) called Solid Work is use to design the wind tunnel. Experiment conducted after build the wind tunnel to find drag coefficient of a sphere. The drag force on a sphere in an air stream was measured at various free stream velocities below 100 m/s. This was done in a low speed wind tunnel using an integral balance system to measure the drag force and a Pitot tube and to measure the velocity. The raw data were processed according to classical equations of fluid mechanics which define the drag coefficient. An impression of fluid field flow around a sphere is also capture using white smoke. Method of analysis the flow in test section was shown by using strings. The experimental results are compared to published results over the range tested. | |
| 650 | 0 | _aWind tunnels | |
| 650 | 0 | _aProduction engineering | |
| 999 |
_aVIRTUA40 _c3683 _d3689 |
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| 999 | _aVTLSSORT0080*0200*0400*0900*1000*2450*2600*3000*5020*5040*5200*6500*6501*9992 | ||