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NACA-TR-713
Internal-flow systems for aircraft
Year: 1941
Abstract: An investigation has been made to determine efficient arrangements for an internal-flow system of an aircraft when such a system operates by itself or in combination with other flow systems. The investigation included a theoretical treatment of the problem and tests in the NACA 5-foot vertical wind tunnel of inlet and outlet openings in a flat plate and in a wing.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:46:59Z | |
| date available | 2017-09-04T15:46:59Z | |
| date copyright | 01/01/1941 | |
| date issued | 1941 | |
| identifier other | PWWUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/49767 | |
| description abstract | An investigation has been made to determine efficient arrangements for an internal-flow system of an aircraft when such a system operates by itself or in combination with other flow systems. The investigation included a theoretical treatment of the problem and tests in the NACA 5-foot vertical wind tunnel of inlet and outlet openings in a flat plate and in a wing. | |
| language | English | |
| title | NACA-TR-713 | num |
| title | Internal-flow systems for aircraft | en |
| type | standard | |
| page | 33 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1941 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AIR | |
| subject keywords | AIRCRAFT | |
| subject keywords | CONFIGURATIONS | |
| subject keywords | DESIGN | |
| subject keywords | FLOW | |
| subject keywords | INLET | |
| subject keywords | INTAKES | |
| subject keywords | TESTS | |
| subject keywords | TUNNEL | |
| subject keywords | WIND |