Research Catalog

Title

Pressure- and temperature-sensitive paint at 0.3-m transonic cryogenic tunnel / A. Neal Watkins [and three others].

Author

Watkins, A. Neal

Publication

Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2015.

Details

Additional Authors

• Langley Research Center, issuing body.
• United States. National Aeronautics and Space Administration, sponsoring body.

Description

1 online resource (20 pages) : color illustrations.

Series Statement

NASA/TM ; 2015-218801

Uniform Title

NASA technical memorandum ; 2015-218801.

Subjects

• Laminar flow airfoils
• Transonic wind tunnels
• Temperature sensitive paints
• Pressure sensitive paints
• Cryogenics

Note

• Title from title screen (viewed on Jan. 5, 2016).
• "September 2015."

Bibliography (note)

• Includes bibliographical references (pages 18-20).

Funding (note)

• Sponsored by the National Aeronautics and Space Administration

Call Number

GPO Internet NAS 1.15:2015-218801

OCLC

marcive933745170

Author

Watkins, A. Neal, author.

Title

Pressure- and temperature-sensitive paint at 0.3-m transonic cryogenic tunnel / A. Neal Watkins [and three others].

Publisher

Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2015.

Type of Content

text

Type of Medium

computer

Type of Carrier

online resource

Series

NASA/TM ; 2015-218801

NASA technical memorandum ; 2015-218801.

Bibliography

Includes bibliographical references (pages 18-20).

Funding

Sponsored by the National Aeronautics and Space Administration 109492.02.07.02.20.01

L-20601

Connect to:

https://purl.fdlp.gov/GPO/gpo64042

Added Author

Langley Research Center, issuing body.

United States. National Aeronautics and Space Administration, sponsoring body.

Gpo Item No.

0830-D (online)

Sudoc No.

NAS 1.15:2015-218801