Johnson, W. G., & Hill, A. S. (1985). Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch.
Chicago Style (17th ed.) CitationJohnson, William G., and Acquilla S. Hill. Pressure Distributions from High Reynolds Number Tests of a Boeing BAC I Airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
MLA (9th ed.) CitationJohnson, William G., and Acquilla S. Hill. Pressure Distributions from High Reynolds Number Tests of a Boeing BAC I Airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.