Cover Image

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 /

Bibliographic Details
Corporate Author: Langley Research Center
Other Authors: Watkins, Anthony Neal
Format: Government Document eBook
Language:English
Published: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
Series:NASA technical memorandum ; 217316.
Subjects:
Pressure measurement.
Pressure sensitive paints.
Flow distribution.
Flight simulation.
Pressure sensors.
Horizontal flight.
Blade tips.
Online Access:https://purl.fdlp.gov/GPO/gpo22695
Description
Item Description:Title from title screen (viewed on May 15, 2012).
"December 2011."
Electronic resource.
Physical Description:1 online resource (18 pages) : color illustrations
Bibliography:Includes bibliographical references (pages 17-18).