DESAIN PELURUS ALIRAN PADA SETTLING CHAMBER TEROWONGAN ANGIN SUPERSONIK
Laboratory scale supersonic wind tunnel has been developed by Flight Physics Group, Faculty of Mechanical and Aerospace Engineering. This wind tunnel was designed to achieve Mach number equal to 2 in the test section, where the aerodynamics characteristics of an object to be tested. To obtain accura...
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| Main Author: | |
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/62014 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |