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Air admixture to exhaust jets
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1953 |
| Description | The problem of thrust increase by air admixture to exhaust jets of rockets, turbojet, ram- and pulse-jet engines is investigated theoretically. The optimum ratio of mixing chamber pressure to ambient pressure and speed range for thrust increase due to air admixture is determined for each type of jet engine. |
| File Size | 1332122 |
| Page Count | 36 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930093873 |
| Archival Resource Key | ark:/13960/t87h5xz3d |
| Language | English |
| Publisher Date | 1953-07-01 |
| Access Restriction | Open |
| Subject Keyword | Engines, Pulse-jet Pumps, Jet Amd Thrust Augmentors Engines, Turbojet Ducts 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 |