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NASA-TM-76710
Influence of the Reynolds number on the normal forces of slender bodies of revolution
Year: 1982
Abstract: Comprehensive force, moment, and pressure distribution measurements as well as flow visualization experiments were carried out to determine the influence of the Reynolds number on nonlinear normal forces of slender bodies of revolution. Experiments were performed in transonic wind tunnels at angles of attack up to 90 deg in the Mach number range 0.5 to 2.2 at variable Reynolds numbers. The results were analysed theoretically and an empirical theory was developed which describes the test results satisfactory.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:57:05Z | |
| date available | 2017-09-04T15:57:05Z | |
| date copyright | 01/01/1982 | |
| date issued | 1982 | |
| identifier other | QZMKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/60408 | |
| description abstract | Comprehensive force, moment, and pressure distribution measurements as well as flow visualization experiments were carried out to determine the influence of the Reynolds number on nonlinear normal forces of slender bodies of revolution. Experiments were performed in transonic wind tunnels at angles of attack up to 90 deg in the Mach number range 0.5 to 2.2 at variable Reynolds numbers. The results were analysed theoretically and an empirical theory was developed which describes the test results satisfactory. | |
| language | English | |
| title | NASA-TM-76710 | num |
| title | Influence of the Reynolds number on the normal forces of slender bodies of revolution | en |
| type | standard | |
| page | 31 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1982 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | BODIES | |
| subject keywords | BOUNDARY | |
| subject keywords | DISTRIBUTION | |
| subject keywords | FLOW | |
| subject keywords | FORCE | |
| subject keywords | FORCES | |
| subject keywords | LAYER | |
| subject keywords | MOMENT | |
| subject keywords | NUMBER | |
| subject keywords | PRESSURE | |
| subject keywords | REVOLUTION | |
| subject keywords | REYNOLDS | |
| subject keywords | SEPARATION | |
| subject keywords | SLENDER | |
| subject keywords | TESTS | |
| subject keywords | TUNNEL | |
| subject keywords | VISUALIZATION | |
| subject keywords | VORTICES | |
| subject keywords | WIND |