HIGH LIFT SURFACE DESIGN PROCEDURES. EXPERIMENTAL VERIFICATION. VOLUME II. THEORETICAL DESIGN AND ANALYSIS.
NORAIR DIV NORTHROP CORP HAWTHORNE CALIF
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The development of four wings which were designed to have specific aerodynamic requirements is described. The wings designed were a high lift wing, a low lift or cruise wing, both of which were smooth, and two flapped wings which were approximations of the smooth wings.