Effect of leading-edge-flap deflection on the wing loads, load distributions , and flap hinge moments of the Douglas X-3 research airplane at transonic speeds

Author: Keener, Earl R.
Additional Authors: McLeod, Norman J.
Year: 1958
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-H58D29
Link: https://digital.library.unt.edu/ark:/67531/metadc64336/

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