Boundary layer control affects performance and structure of aircraft to such extent that it has to be considered in preliminary design of vehicle; factors to be included in parametric studies; primitive design method suggested is explained for case of subsonic STOL transport; high lift BLC systems and correlations of available data; state of art suggests flexible concept of multiple cell system.
Design considerations for BLC STOL airplanes
Aero/Space Eng
Aero/Space Engineering ; 17 , n 10
1958
7 pages
Article (Journal)
English
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