| dc.contributor.author | Kumar, Rajesh | |
| dc.date.accessioned | 2026-07-07T05:23:58Z | |
| dc.date.available | 2026-07-07T05:23:58Z | |
| dc.date.issued | 2026-05 | |
| dc.identifier.govdoc | NB19284 | |
| dc.identifier.uri | http://127.0.0.1/xmlui/handle/123456789/17537 | |
| dc.language.iso | en | en_US |
| dc.publisher | IIT Kharagpur | en_US |
| dc.subject | Urans Simulation | en_US |
| dc.subject | Combustor Configuration | en_US |
| dc.subject | Pulses Steepen | en_US |
| dc.subject | Scramjet Engines | en_US |
| dc.title | Effects of Combustor Configurations on Combustion Modes and Flow Dynamics in Scramjet Engines | en_US |
| dc.type | Thesis | en_US |