Research Catalog

Title

Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel / Anthony Neal Watkins ... [and others].

Publication

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]

Details

Additional Authors

• Watkins, Anthony Neal.
• Langley Research Center.

Description

1 online resource (18 pages) : color illustrations.

Series Statement

NASA/TM ; 2011-217316

Uniform Title

NASA technical memorandum ; 217316.

Subject

• Pressure measurement
• Pressure sensitive paints
• Flow distribution
• Flight simulation
• Pressure sensors
• Horizontal flight
• Blade tips

Note

• Title from title screen (viewed on May 15, 2012).
• "December 2011."

Bibliography (note)

• Includes bibliographical references (pages 17-18).

Call Number

GPO Internet NAS 1.15:2011-217316

OCLC

marcive793599684

Title

Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel / Anthony Neal Watkins ... [and others].

Publisher

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]

Type of Content

text

Type of Medium

computer

Type of Carrier

online resource

Series

NASA/TM ; 2011-217316

NASA technical memorandum ; 217316.

Bibliography

Includes bibliographical references (pages 17-18).

Funding

L-20095

877868.02.07.07.06.03.01

Connect to:

https://purl.fdlp.gov/GPO/gpo22695

Added Author

Watkins, Anthony Neal.

Langley Research Center.

Gpo Item No.

0830-D (online)

Sudoc No.

NAS 1.15:2011-217316