MIT WTTbgbmgfbg
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![Page 1: MIT WTTbgbmgfbg](https://reader034.fdocuments.us/reader034/viewer/2022051223/56d6c0651a28ab30169a3437/html5/thumbnails/1.jpg)
An airplane model mounted in test section with internal strain gauge balance
Aerodynamic Laboratory Facilities Faculty –in – charge : Dr. K.M. Parammasivam & Dr. C.Senthil Kumar
Subsonic wind tunnel Facility with Test Section size 3’ x 4’ x 6’. Max. Speed in test section 60m/s
Side view of airplane model mounted in test section with strain gauge balance
![Page 2: MIT WTTbgbmgfbg](https://reader034.fdocuments.us/reader034/viewer/2022051223/56d6c0651a28ab30169a3437/html5/thumbnails/2.jpg)
Subsonic wind tunnel facility with test section size 1’ x 1’ x 3’. Max. speed in test
section 25 m/s. 16 channel scanner for pressure
measurements
3 component and 6 component internal strain gauge balances for aerodynamic force and
moment measurements
Electronically controlled angle of attack changing mechanism for
aerodynamic models in wind tunnel test section