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Operating characteristics of the langley mach 7 scramjet test facility
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sabol, A. P. Guy, R. W. Torrence, M. G. Mueller, J. N. |
| Copyright Year | 1981 |
| Description | Operating characteristics of the Langley Mach 7 Scramjet Test Facility are described. The facility is designed for testing airframe integrated scramjet (supersonic combustion ramjet) engine models. Features include duplication of the flight Mach number total enthalpy, flight altitude simulation, and simulation of engine airframe integration effects such a bow shock wave precompression and boundary layer ingestion by the engine. Data obtained from facility calibration and from tests of a hydrogen burning, airframe integrated scramjet are discussed. An adverse interaction between the facility flow and the scramjet engine flow during combustion of the fuel is described. |
| File Size | 2518928 |
| Page Count | 55 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810011555 |
| Archival Resource Key | ark:/13960/t0vq7rn9d |
| Language | English |
| Publisher Date | 1981-03-01 |
| Access Restriction | Open |
| Subject Keyword | Research And Support Facilities (air) Fuel Combustion Turbulent Flow Wind Tunnels Arc Heating Enthalpy Supersonic Combustion Ramjet Engines Aerodynamics Mach Number Flight Simulation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
