Presentation of all currently available force test data for airfoils obtained under same test conditions in Langley 24-in. high speed tunnel; airfoils tested over Mach number range from 0.3 to 0.8.
Aerodynamic characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.8
Nat Advisory Committee Aeronautics -- Tech Note
1948
86 pages
Report
English
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