It is shown that in consideration of aircraft equipped with turbo-unit, necessity for providing air intake for turbine can be turned to advantage by arranging intake inlet to exert influence on boundary layer air flow; inherently applicable to jet propelled aircraft.
Boundary layer control
Flight
Flight ; 45 , n 1837
1944
3 pages
Article (Journal)
English
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Engineering Index Backfile | 1951
Engineering Index Backfile | 1955
|Laminar-Boundary-Layer Control
NTIS | 1957
|