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Oblique detonation wave ramjet
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Morrison, R. B. |
| Copyright Year | 1980 |
| Description | Two conceptual designs of the oblique detonation wave ramjet are presented. The performance is evaluated for stoichiometric hydrogen-air equivalence ratios of phi = 1/3, 2/3 and 1 for a range of flight Mach numbers from 6 to 10. |
| File Size | 2455245 |
| Page Count | 88 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800005874 |
| Archival Resource Key | ark:/13960/t1hj1b937 |
| Language | English |
| Publisher Date | 1980-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Shock Wave Attenuation Hydrogen Fuels Ramjet Engines Engine Design Jet Thrust Oblique Shock Waves Detonation Waves Diffusers Fuel Injection Combustion Chambers Propulsion System Configurations Fuel-air Ratio Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |