درباره ما
NACA-TN-2528
A method for predicting the upwash angles induced at the propeller plane of a combination of bodies with an upswept wing
Year: 1951
Abstract: A method has been developed the horizontal center line of the propeller disk of the twin-engine airplane considered in NACA TN 2192, 1950. The method treats each component separately and includes approximations for the interference effects of the other components. Lifting-line theory was used to determine the wing-induced upwash angles. The theory used for the nacelle is an extension of the airship theory of NACA TM 574, 1930. The fuselage-induced upwash angles were determined by means of a solution for the transverse flow about an infinite elliptic cylinder.
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:28:57Z | |
| date available | 2017-09-04T16:28:57Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | UHLUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/92182 | |
| description abstract | A method has been developed the horizontal center line of the propeller disk of the twin-engine airplane considered in NACA TN 2192, 1950. The method treats each component separately and includes approximations for the interference effects of the other components. Lifting-line theory was used to determine the wing-induced upwash angles. The theory used for the nacelle is an extension of the airship theory of NACA TM 574, 1930. The fuselage-induced upwash angles were determined by means of a solution for the transverse flow about an infinite elliptic cylinder. | |
| language | English | |
| title | NACA-TN-2528 | num |
| title | A method for predicting the upwash angles induced at the propeller plane of a combination of bodies with an upswept wing | en |
| type | standard | |
| page | 25 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext |