A Characterized Status Report on Pulse Detonation Engine
Pulse Detonation Engine (PDE), is an exciting propulsion technology for the future and has been able to seek considerable attention over the last era. It has the potential to work efficiently in the modern cosmos. It works on a Humphrey cycle offering a great opportunity, which outweighs the convent...
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2019-06-01
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| Series: | INCAS Bulletin |
| Subjects: | |
| Online Access: | http://bulletin.incas.ro/files/dogra_singh_jindal__vol_11_iss_2.pdf |
| _version_ | 1831548667258994688 |
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| author | Bharat Ankur DOGRA Mehakveer SINGH T. K. JINDAL |
| author_facet | Bharat Ankur DOGRA Mehakveer SINGH T. K. JINDAL |
| author_sort | Bharat Ankur DOGRA |
| collection | DOAJ |
| description | Pulse Detonation Engine (PDE), is an exciting propulsion technology for the future and has been able to seek considerable attention over the last era. It has the potential to work efficiently in the modern cosmos. It works on a Humphrey cycle offering a great opportunity, which outweighs the conventional Brayton cycle. The operating cycle of PDE starts with the fuel-oxidizer mixture, combustion and DDT followed by purging. The PDE combustion process, which is a unique process, leads to consistent and repeatable detonation waves. This pulsed detonation combustion process causes rapid burning of the fuel-oxidizer mixture, which cannot be seen in any other combustion process as it is a thousand times faster than any other mode of combustion. PDE not only holds the capability of running effectively up to Mach 5 but it also changes the technicalities in space propulsion. The present study deals with the categorization of design approach, thermal analysis, performance analysis, fuel-based analysis, PDE combustors, detonation propagation, experimentation analysis, valving techniques, ignition studies, parameters & specification optimization, instrumentation, thrusters, parameters affecting specific impulse & thrust, hybrid PDE’s & turbine integration. |
| first_indexed | 2024-12-17T02:24:24Z |
| format | Article |
| id | doaj.art-c254e50bef0a405a8ea09147caa1d6c9 |
| institution | Directory Open Access Journal |
| issn | 2066-8201 2247-4528 |
| language | English |
| last_indexed | 2024-12-17T02:24:24Z |
| publishDate | 2019-06-01 |
| publisher | National Institute for Aerospace Research “Elie Carafoli” - INCAS |
| record_format | Article |
| series | INCAS Bulletin |
| spelling | doaj.art-c254e50bef0a405a8ea09147caa1d6c92022-12-21T22:07:10ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282019-06-01111698310.13111/2066-8201.2019.11.2.6A Characterized Status Report on Pulse Detonation EngineBharat Ankur DOGRA0Mehakveer SINGH1T. K. JINDAL2Aerospace Engineering Department, Punjab Engineering College, (Deemed to be University), Sector-12, Chandigarh, 160012- India, mechanicalerankur906@gmail.com*Aerospace Engineering Department, Punjab Engineering College, (Deemed to be University), Sector-12, Chandigarh, 160012- India, mehakveersingh11@gmail.comAerospace Engineering Department, Punjab Engineering College, (Deemed to be University), Sector-12, Chandigarh, 160012- India, tkjindal@pec.ac.inPulse Detonation Engine (PDE), is an exciting propulsion technology for the future and has been able to seek considerable attention over the last era. It has the potential to work efficiently in the modern cosmos. It works on a Humphrey cycle offering a great opportunity, which outweighs the conventional Brayton cycle. The operating cycle of PDE starts with the fuel-oxidizer mixture, combustion and DDT followed by purging. The PDE combustion process, which is a unique process, leads to consistent and repeatable detonation waves. This pulsed detonation combustion process causes rapid burning of the fuel-oxidizer mixture, which cannot be seen in any other combustion process as it is a thousand times faster than any other mode of combustion. PDE not only holds the capability of running effectively up to Mach 5 but it also changes the technicalities in space propulsion. The present study deals with the categorization of design approach, thermal analysis, performance analysis, fuel-based analysis, PDE combustors, detonation propagation, experimentation analysis, valving techniques, ignition studies, parameters & specification optimization, instrumentation, thrusters, parameters affecting specific impulse & thrust, hybrid PDE’s & turbine integration.http://bulletin.incas.ro/files/dogra_singh_jindal__vol_11_iss_2.pdfPulse Detonation Engine (PDE)Deflagration to Detonation Transition (DDT)Rotating Detonation Engine (RDE)specific impulseShchelkin spiralRotating Detonation Wave Engine (RDWE) |
| spellingShingle | Bharat Ankur DOGRA Mehakveer SINGH T. K. JINDAL A Characterized Status Report on Pulse Detonation Engine INCAS Bulletin Pulse Detonation Engine (PDE) Deflagration to Detonation Transition (DDT) Rotating Detonation Engine (RDE) specific impulse Shchelkin spiral Rotating Detonation Wave Engine (RDWE) |
| title | A Characterized Status Report on Pulse Detonation Engine |
| title_full | A Characterized Status Report on Pulse Detonation Engine |
| title_fullStr | A Characterized Status Report on Pulse Detonation Engine |
| title_full_unstemmed | A Characterized Status Report on Pulse Detonation Engine |
| title_short | A Characterized Status Report on Pulse Detonation Engine |
| title_sort | characterized status report on pulse detonation engine |
| topic | Pulse Detonation Engine (PDE) Deflagration to Detonation Transition (DDT) Rotating Detonation Engine (RDE) specific impulse Shchelkin spiral Rotating Detonation Wave Engine (RDWE) |
| url | http://bulletin.incas.ro/files/dogra_singh_jindal__vol_11_iss_2.pdf |
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