United States. National Advisory Committee for Aeronautics. (1938). Calculation of chord-wise load distribution over air℗-foil sections with plain, split, or serially hinged trailing℗--edge flaps. [s.n.].
Chicago Style (17th ed.) CitationUnited States. National Advisory Committee for Aeronautics. Calculation of Chord-wise Load Distribution over Air℗-foil Sections with Plain, Split, or Serially Hinged Trailing℗--edge Flaps. [Washington]: [s.n.], 1938.
MLA (9th ed.) CitationUnited States. National Advisory Committee for Aeronautics. Calculation of Chord-wise Load Distribution over Air℗-foil Sections with Plain, Split, or Serially Hinged Trailing℗--edge Flaps. [s.n.], 1938.
Warning: These citations may not always be 100% accurate.