Tests made to define characteristics of two of configurations used in comprehensive investigation of control surface characteristics and also to provide additional data for comparison with previous boundary layer analyses.
Wind-tunnel investigation of boundary layer on NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps
Nat Advisory Committee Aeronautics -- Tech Note
1948
53 pages
Bibliography
Report
English
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Engineering Index Backfile | 1948
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