DESIGN AND ANALYSIS OF WAVERIDER SCRAMJET INTAKE USING COMPUTATIONAL FLUID DYNAMICS
This thesis discussed waverider scramjet intake design and analysis for hypersonic flight conditions purposes, specifically within velocity of Mach 11.5-12.5 and altitude of 100000 ft-140000 ft. Scramjet engine generates thrust by decelerating hypersonic flow to supersonic flow passing a combustion....
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| Format: | Final Project |
| Language: | Indonesia |
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| Online Access: | https://digilib.itb.ac.id/gdl/view/74662 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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