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Surface Effect Take-Off and Landing System (SETOLS) Subsonic Static Stability Out of Ground Effect
| Content Provider | Semantic Scholar |
|---|---|
| Author | Davidson, H. D. Frank, Lawrence A. |
| Copyright Year | 1972 |
| Abstract | Abstract : The effect of a deployed air cushion landing gear on the stability of a high performance aircraft was studied at the Naval Ship Research and Development Center's 8 x 10 foot subsonic wind tunnel. Air cushion designs submitted by Bell Aerospace Corporation and Boeing were fitted to a ten percent scale A-4E and air cushions designed by Goodyear (two configurations), San Diego Aircraft Engineering Incorporated (SANDAIRE), and Bell were fitted to a ten percent scale F-8C. The effects of the air cushion landing gear ranged from minor destabilization, to very detrimental destabilization on both aircraft in the landing approach configuration. |
| File Format | PDF HTM / HTML |
| DOI | 10.21236/ad0763365 |
| Alternate Webpage(s) | http://www.dtic.mil/dtic/tr/fulltext/u2/763365.pdf |
| Alternate Webpage(s) | https://doi.org/10.21236/ad0763365 |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |
