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NACA-TN-4405
Free-flight investigation to determine the drag of flat - and vee - windshield canopies on a parabolic fuselage with and without transonic indentation between Mach numbers of 0.75 and 1.35
Year: 1958
Abstract: A free-flight investigation was conducted between Mach numbers of 0.75 and 1.35 to determine the effects on model total drag and pressure drag of (a) canopy location (along a parabolic body of revolution), (b) canopy windshield shape, (c) canopy fineness ratio, and (d) transonic area-rule indentation.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:57:56Z | |
| date available | 2017-09-04T15:57:56Z | |
| date copyright | 01/01/1958 | |
| date issued | 1958 | |
| identifier other | RBOUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/61155 | |
| description abstract | A free-flight investigation was conducted between Mach numbers of 0.75 and 1.35 to determine the effects on model total drag and pressure drag of (a) canopy location (along a parabolic body of revolution), (b) canopy windshield shape, (c) canopy fineness ratio, and (d) transonic area-rule indentation. | |
| language | English | |
| title | NACA-TN-4405 | num |
| title | Free-flight investigation to determine the drag of flat - and vee - windshield canopies on a parabolic fuselage with and without transonic indentation between Mach numbers of 0.75 and 1.35 | en |
| type | standard | |
| page | 35 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1958 | |
| contenttype | fulltext |