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Impact of dissociation and sensible heat release on pulse detonation and gas turbine engine performance
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Povinelli, Louis A. |
| Copyright Year | 2001 |
| Description | A thermodynamic cycle analysis of the effect of sensible heat release on the relative performance of pulse detonation and gas turbine engines is presented. Dissociation losses in the PDE (Pulse Detonation Engine) are found to cause a substantial decrease in engine performance parameters. |
| File Size | 469658 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20010093212 |
| Archival Resource Key | ark:/13960/t6450mz0d |
| Language | English |
| Publisher Date | 2001-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Propulsion System Performance Thermal Dissociation Gas Turbine Engines Thermodynamic Cycles Engine Tests Pulse Detonation Engines Heat Transfer Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
