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NACA-TR-1307
Lift and center of pressure of wing-body-tail combinations at subsonic, transonic, and supersonic speeds
Year: 1957
Abstract: A method is presented for calculating the lift and centers of pressure of wing-body and wing-body-tail combinations at subsonic, transonic, and supersonic speeds. A set of design charts and a computing table are presented which reduce the computations to routine operations. Comparison between the estimated and experimental characteristics for a number of wing-body and wing-body-tail combinations shows correlation to within or - 10 percent on lift and to within about or - 0.02 of the body length on center of pressure.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:58:53Z | |
| date available | 2017-09-04T17:58:53Z | |
| date copyright | 01/01/1957 | |
| date issued | 1957 | |
| identifier other | FSUYYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho162s6596FCDCAC4261590-%20Naval%20Facilities%20E/handle/yse/182056 | |
| description abstract | A method is presented for calculating the lift and centers of pressure of wing-body and wing-body-tail combinations at subsonic, transonic, and supersonic speeds. A set of design charts and a computing table are presented which reduce the computations to routine operations. Comparison between the estimated and experimental characteristics for a number of wing-body and wing-body-tail combinations shows correlation to within or - 10 percent on lift and to within about or - 0.02 of the body length on center of pressure. | |
| language | English | |
| title | NACA-TR-1307 | num |
| title | Lift and center of pressure of wing-body-tail combinations at subsonic, transonic, and supersonic speeds | en |
| type | standard | |
| page | 70 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1957 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AERODYNAMICS | |
| subject keywords | AIRCRAFT | |
| subject keywords | BODIES | |
| subject keywords | BODY | |
| subject keywords | CENTER | |
| subject keywords | CIRCULAR | |
| subject keywords | COMPONENTS | |
| subject keywords | COMPUTATIONAL | |
| subject keywords | CONFIGURATIONS | |
| subject keywords | CYLINDERS | |
| subject keywords | CYLINDRICAL | |
| subject keywords | DYNAMICS | |
| subject keywords | FLUID | |
| subject keywords | INTERACTIONAL | |
| subject keywords | INTERFERENCE | |
| subject keywords | LIFT | |
| subject keywords | MISSILE | |
| subject keywords | PRESSURE | |
| subject keywords | RECTANGULAR | |
| subject keywords | SPEED | |
| subject keywords | SUBSONIC | |
| subject keywords | SUPERSONIC | |
| subject keywords | SURFACES | |
| subject keywords | TAIL | |
| subject keywords | TRANSONIC | |
| subject keywords | TRAPEZOIDAL | |
| subject keywords | WING | |
| subject keywords | WINGS |