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Ground effects on the longitudinal characteristics of two models with wings having low aspect ratio and pointed tips (Document No: 19930084743)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1957 |
| Description | Wind-tunnel tests were conducted to determine the ground effects on a tailless model with a wing of aspect ratio 2 and infinite taper, and on a tailed model with a triangular wing of aspect ratio 3, with flaps. Control-surface hinge moments were measured on the tailless model. The results are compared with the predictions of the theory of Tani, et al. |
| File Size | 20049149 |
| Page Count | 49 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930084743 |
| Archival Resource Key | ark:/13960/t3zs7g757 |
| Language | English |
| Publisher Date | 1957-07-01 |
| Access Restriction | Open |
| Subject Keyword | Controls, Flap-type - Complete Wings Wing-fuselage Combinations - Airplanes Tail-wing-fuselage Combinations - Airplanes Control, Hinge Moments Control, Longitudinal Flaps, Trailing-edge - Complete Wings Stability, Longitudinal - Static 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 |