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Stratified charge rotary aircraft engine technology enablement program
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Badgley, P. R. Irion, C. E. Myers, D. M. |
| Copyright Year | 1985 |
| Description | The multifuel stratified charge rotary engine is discussed. A single rotor, 0.7L/40 cu in displacement, research rig engine was tested. The research rig engine was designed for operation at high speeds and pressures, combustion chamber peak pressure providing margin for speed and load excursions above the design requirement for a high is advanced aircraft engine. It is indicated that the single rotor research rig engine is capable of meeting the established design requirements of 120 kW, 8,000 RPM, 1,379 KPA BMEP. The research rig engine, when fully developed, will be a valuable tool for investigating, advanced and highly advanced technology components, and provide an understanding of the stratified charge rotary engine combustion process. |
| File Size | 7058568 |
| Page Count | 120 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850012853 |
| Archival Resource Key | ark:/13960/t5m953h2p |
| Language | English |
| Publisher Date | 1985-01-31 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Performance Tests Internal Combustion Engines Rotary Engines Product Development Aircraft Engines Fuel Injection Design Analysis Stratification Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
