Planing-surface Tests at Large Froude Numbers - Airfoil Comparison (1938)
NASA Technical Reports Server (NTRS) · leaf 21
Figs. 1,2,3,4,5,6,7,8,9 N.A.C.A. Technical Memorandum No. 848 £ H '////////// -k Figure 6.- Effective angle of attack enlarged byApw as result of turbulent flow on the planing sur- Figure 1.- Test quantities used in face. … Figure 5.- Velocity distribution flow on long planing surface and of turbulent flow at airfoil, planing surface.
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