Model tested as high wing, midwing, and low wing monoplane; for each wing location tests were made with two amounts of dihedral and with partial span split flaps; results are presented and discussed.
Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. II. Rectangular, N.A.C.A. 23012 wing with circular fuselage and fin
Nat Advisory Committee Aeronautics -- Tech Note
1939
Bibliography
Report
Englisch
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Pressure distribution over N.A.C.A. 23012 airfoil with N.A.C.A. 23012 external-airfoil flap
Engineering Index Backfile | 1938
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