Novel Characteristics of Subsonic Coflowing Jets With Varying Lip Thickness
Effect of Mach number on coflowing jet at lip thickness of 0.2 Dp, 1.0 Dp and 1.5 Dp (where Dp is primary nozzle exit diameter, 10 mm) at Mach numbers 1.0, 0.8 and 0.6 were studied experimentally. It was found that an increase in Mach number does not have any profound effect on axial total and stati...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
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Departamento de Ciência e Tecnologia Aeroespacial
2020-06-01
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| Series: | Journal of Aerospace Technology and Management |
| Subjects: | |
| Online Access: | https://www.scielo.br/pdf/jatm/v12/2175-9146-jatm-12-e2520.pdf |