Hybrid Wave Rotor Electric Aero Propulsion
| dc.contributor.author | Nalim, M. Razi | |
| dc.contributor.author | Bane, Sally P.M. | |
| dc.contributor.author | Khan, M. Javed | |
| dc.contributor.author | Jagannath, Ravichandra | |
| dc.date.accessioned | 2019-09-27T21:23:33Z | |
| dc.date.available | 2019-09-27T21:23:33Z | |
| dc.date.issued | 2014 | |
| dc.description.abstract | Purpose: The goal of this project was to investigate the proposed hybrid wave-rotor electric aero-propulsion concept (HyWREAP). The tasks were to perform flow and combustion analysis of the pressure-gain, wave-rotor combustor (WRC) turbine concept, and investigate benefits for the most likely flight application of HyWREAP. | en_US |
| dc.identifier.citation | Nalim, M. Razi. (2014). Hybrid Wave-Rotor Electric Aero-Propulsion (HyWREAP). Presented at the 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. | en_US |
| dc.identifier.uri | https://hdl.handle.net/1805/20981 | |
| dc.language.iso | en_US | en_US |
| dc.subject | Hybrid wave-rotor electric aero-propulsion concept (HyWREAP) | en_US |
| dc.subject | Hybrid propulsion | en_US |
| dc.subject | Airplanes | en_US |
| dc.subject | Combustion turbine engines | en_US |
| dc.subject | Wave rotor combustion turbine (WRCT) | en_US |
| dc.title | Hybrid Wave Rotor Electric Aero Propulsion | en_US |
| dc.type | Other | en_US |