Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers)
| dc.contributor.author | Campion, B. S. | |
| dc.date.accessioned | 2012-09-13T15:34:42Z | |
| dc.date.available | 2012-09-13T15:34:42Z | |
| dc.date.issued | 1954-01 | |
| dc.description.abstract | The effects if distortion on the longitudinal stability of swept wing aircraft at high speeds (sub-critical Mach numbers) are considered on a quasi-static basis. The method employed is based on the theory of Gates and Lyon but involves some extension of this theory. | en_UK |
| dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/7579 | |
| dc.language.iso | en | en_UK |
| dc.publisher | College of Aeronautics, Cranfield | en_UK |
| dc.relation.ispartofseries | College Reports | en_UK |
| dc.relation.ispartofseries | 77 | en_UK |
| dc.title | Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers) | en_UK |
| dc.type | Report | en_UK |