fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel
By: Pierce L. Lawing, Jerry B. Adcock, and Charles L. Ladson
Contributors: Adcock, Jerry B; Ladson, Charles L; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical paper -- 1752
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 18
Subjects: Aerodynamics, Transonic; Wind tunnels -- Ground simulators -- Testing; Low temperature engineering
Notes: "Langley Research Center."

Nov. 1980

Includes bibliograpahical references