A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel / Pierce L. Lawing, Jerry B. Adcock, and Charles L. Ladson.

Format:

• Book
• Government document

Author/Creator:

• Lawing, Pierce L., author.
• Adcock, Jerry B., author.
• Ladson, Charles L., author.

Contributor:

• Langley Research Center
• United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.

Series:

• NASA technical paper ; 1752.
• NASA technical paper ; 1752

Language:

English

Subjects (All):

• Aerodynamics, Transonic.
• Wind tunnels--Ground simulators--Testing.
• Low temperature engineering.

Genre:

• Online resources.

Physical Description:

1 online resource (18 pages) : illustrations

Place of Publication:

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

Notes:

• Title from title screen (viewed on August 17, 2016).
• "November 1980."
• "Performing Organization: NASA Langley Research Center"--Report documentation page
• Includes bibliographical references (page 11).

Other Format:

• Print version: Lawing, Pierce L. Fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel
• Microfiche version: Lawing, Pierce L. Fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel

OCLC:

761455916