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Reversed cowl-flap thrust augmentor
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Cheng, D. Y. |
| Copyright Year | 1974 |
| Description | Inlet mouthpiece with variable geometry improves low-speed performance of inlet (or ejector) of jet engines by use of reversed cowl-flap mechanism. Flaps can be adjusted mechanically or system can be operated with pressure taps set so pressure on inlet face is always smaller than pressure on back of inlet. |
| File Size | 76669 |
| Page Count | 1 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740000046 |
| Archival Resource Key | ark:/13960/t1rg0hf55 |
| Language | English |
| Publisher Date | 1974-05-01 |
| Access Restriction | Open |
| Subject Keyword | Cowlings Jet Flow Inlet Pressure Flaps Control Surfaces Thrust Augmentation Aircraft Launching Devices Landing Aids Intake Systems Jet Engines 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 |