A profile-drag investigation in flight on an experimental fighter-type airplane the North American XP-51
Description: Report discussing the results of an investigation of the North American XP-51 and its low-drag airfoils. Several surface conditions were tested and the profile-drag coefficients were determined. The surface that was smoothened and faired by filling and sanding had the lowest profile-drag coefficient.
Date: November 1942
Creator: Zalovcik, John A.
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Partner: UNT Libraries Government Documents Department