Investigations carried out by Guggenheim Aeronautics Laboratory at California Institute of Technology on effects of boundary layer transition phenomena and surface roughness on drag; results of this investigation show that apparatus developed for measuring wing section drags in flight is practical and is amenable to quick adaptation to full scale airplane. Before Inst Aeronautical Sciences.
Boundary layer and wake survey measurements in flight and in wind tunnel
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 7 , n 10 ; p 425-433
1940
9 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
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