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NACA-TR-D-745
High-Speed Tests of Conventional Radial-Engine Cowlings
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:30:04Z | |
| date available | 2017-09-04T15:30:04Z | |
| date copyright | 01/01/1942 | |
| date issued | 1942 | |
| identifier other | NZONEEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/31431 | |
| description abstract | The drag characteristics of eight radial-engine cowlings have been determined over a wide speed range in the NACA 8-foot high-speed wind tunnel. The pressure distribution over all cowlings was measured, to and above the speed of the compressibility burble, as an aid in interpreting the force tests. One-fifth-scale models of radial-engine cowlings on a wing-nacelle combination were used in the tests. | |
| language | English | |
| title | NACA-TR-D-745 | num |
| title | High-Speed Tests of Conventional Radial-Engine Cowlings | en |
| type | standard | |
| page | 13 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1942 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC DRAG | |
| subject keywords | AIRCRAFT ENGINES | |
| subject keywords | COMPRESSIVE STRENGTH | |
| subject keywords | HIGH SPEED | |
| subject keywords | PRESSURE DISTRIBUTION | |
| subject keywords | SCALE MODELS | |
| subject keywords | WIND TUNNEL MODELS | |
| subject keywords | WIND TUNNEL TESTS |
