Lawing, P. L., Adcock, J. B., & Ladson, C. L. (1980). A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch.
Chicago Style (17th ed.) CitationLawing, Pierce L., Jerry B. Adcock, and Charles L. Ladson. A Fan Pressure Ratio Correlation in Terms of Mach Number and Reynolds Number for the Langley 0.3-Meter Transonic Cryogenic Tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980.
MLA (9th ed.) CitationLawing, Pierce L., et al. A Fan Pressure Ratio Correlation in Terms of Mach Number and Reynolds Number for the Langley 0.3-Meter Transonic Cryogenic Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980.