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Theoretical and experimental study on the ejector augmented jet flap
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stewart, H. J. |
| Copyright Year | 1974 |
| Description | The analytical concept used in determining the characteristics of jet flap or related propulsive systems suitable for VTOL and STOL applications was examined. The configuration chosen was a two dimensional wing with a biplane flap, having a jet injected on the upper surface of the wing at the flap hinge axis and discharging into the channel between the two elements of the flap. The experimental work was conducted in a two dimensional test installation in a subsonic wind tunnel. The model description, the test conditions, and a summary of the experimental results are presented. |
| File Size | 10002419 |
| Page Count | 259 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750009224 |
| Archival Resource Key | ark:/13960/t3615t19f |
| Language | English |
| Publisher Date | 1974-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Subsonic Wind Tunnels Jet Mixing Flow Wind Tunnel Tests Aerodynamic Coefficients Short Takeoff Aircraft Jet Flaps Two Dimensional Flow Aerodynamic Characteristics Lift Augmentation Vertical Takeoff Aircraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
