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MIL-B-81366
BOUNDARY LAYER CONTROL SYSTEM; PRESSURE
Organization:
NAVY - AS - Naval Air Systems Command
Year: 1966
Abstract: This specification covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff. Intended Use: The boundary layer control system is intended for use in turbo-jet and turbo-prop aircraft to increase the aerodynamic lift of the wings and flaps during approach, landing, and takeoff.
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| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T18:37:45Z | |
| date available | 2017-09-04T18:37:45Z | |
| date copyright | 04/04/1966 | |
| date issued | 1966 | |
| identifier other | JODPDAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho4703AF67081DAC4/handle/yse/219576 | |
| description abstract | This specification covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff. Intended Use: The boundary layer control system is intended for use in turbo-jet and turbo-prop aircraft to increase the aerodynamic lift of the wings and flaps during approach, landing, and takeoff. | |
| language | English | |
| title | MIL-B-81366 | num |
| title | BOUNDARY LAYER CONTROL SYSTEM; PRESSURE | en |
| type | standard | |
| page | 6 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1966 | |
| contenttype | fulltext |