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NACA-RM-A51C14
A semi-empirical method for calculating the pitching moment of bodies of revolution at low Mach numbers
Year: 1951
Abstract: A semiempirical method, in which potential theory is arbitrarily combined with an approximate viscous theory, for calculating the aerodynamic pitching moments for bodies of revolution is presented. The method can also be used for calculating the lift and drag forces. The calculated and experimental force and moment characteristics of 15 bodies of revolution are compared.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:06:51Z | |
| date available | 2017-09-04T18:06:51Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | GNMCWDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/189806 | |
| description abstract | A semiempirical method, in which potential theory is arbitrarily combined with an approximate viscous theory, for calculating the aerodynamic pitching moments for bodies of revolution is presented. The method can also be used for calculating the lift and drag forces. The calculated and experimental force and moment characteristics of 15 bodies of revolution are compared. | |
| language | English | |
| title | NACA-RM-A51C14 | num |
| title | A semi-empirical method for calculating the pitching moment of bodies of revolution at low Mach numbers | en |
| type | standard | |
| page | 28 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | BODIES | |
| subject keywords | FLOW | |
| subject keywords | THEORY | |
| subject keywords | VISCOUS |