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 /

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 /

Saved in:

Bibliographic Details
Imprint:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
Description:	1 online resource (18 p.) : col. ill.
Language:	English
Series:	NASA/TM ; 2011-217316 NASA technical memorandum ; 217316.
Subject:	Pressure -- Measurement. Pressure transducers.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/8832487

Hidden Bibliographic Details
Other authors / contributors:	Watkins, Anthony Neal. Langley Research Center.
Notes:	Title from title screen (viewed on May 15, 2012). "December 2011." Includes bibliographical references (p. 17-18). L-20095 877868.02.07.07.06.03.01
GPO item no.:	0830-D (online)
Govt.docs classification:	NAS 1.15:2011-217316

Description
Item Description:	Title from title screen (viewed on May 15, 2012). "December 2011."
Physical Description:	1 online resource (18 p.) : col. ill.
Bibliography:	Includes bibliographical references (p. 17-18).