Investigation of Flow Field Around the Pointed Cowl Air Intake at Mach 2.0
Experiments and computational studies were carried out to get an understanding of the flow field around a rectangular supersonic intake with pointed cowl shape. Experiments include quantitative pressure measurements and flow visualization studies by using schlieren techniques. The effects of the pre...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Sciendo
2017-12-01
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| Series: | Transport and Aerospace Engineering |
| Subjects: | |
| Online Access: | https://doi.org/10.1515/tae-2017-0021 |