SAE AS81366A
Withdrawn
Boundary Layer Control System; Pressure
Hardcopy , PDF
English
07-02-2004
07-02-2004
NOTICE
1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY (NOT APPLICABLE)
6 NOTES
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.
| DocumentType |
Standard
|
| Pages |
7
|
| PublisherName |
SAE International
|
| Status |
Withdrawn
|
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.
| MIL-B-81365 Base Document:1966 | Bleed Air Systems, General Specification for |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
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