A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel

MLA

Lawing, 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. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.

APA

Lawing, P., Adcock, J., Ladson, C., Langley Research Center & United States. (1980). 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.

Chicago

Lawing, Pierce L., Jerry B. Adcock, Charles L. Ladson, Langley Research Center and United States. 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, November 1980.