Investigation in Langley 300-mph 7- by 10-ft tunnel to determine effects of various sizes and shapes of end plates on aileron characteristics and on aerodynamic characteristics in pitch and yaw of swept wings.
Effect of end plates on swept wings at low speed
Nat Advisory Committee Aeronautics -- Tech Note
1950
60 pages
Illustrations, Diagrams, Graphs
Aufsatz (Zeitschrift)
Englisch
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