United States. National Advisory Committee for Aeronautics. (1937). Fuselage-drag tests in the variable-density wind tunnel: Streamline bodies of revolution, fineness ratio of 5. [s.n.].
Chicago Style (17th ed.) CitationUnited States. National Advisory Committee for Aeronautics. Fuselage-drag Tests in the Variable-density Wind Tunnel: Streamline Bodies of Revolution, Fineness Ratio of 5. [Washington]: [s.n.], 1937.
MLA (9th ed.) CitationUnited States. National Advisory Committee for Aeronautics. Fuselage-drag Tests in the Variable-density Wind Tunnel: Streamline Bodies of Revolution, Fineness Ratio of 5. [s.n.], 1937.
Warning: These citations may not always be 100% accurate.