Langley 16-ft. transonic tunnel pressure sensitive paint system /

Langley 16-ft. transonic tunnel pressure sensitive paint system /

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Bibliographic Details
Imprint:	Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, 2001.
Description:	15 p. : ill. ; 28 cm.
Language:	English
Series:	NASA TM- ; 2001-211017 NASA technical memorandum ; 2001-211017.
Subject:	Fluid dynamic measurements. Fluid dynamics. Transonic wind tunnels. Fluid dynamic measurements. Fluid dynamics. Transonic wind tunnels.
Format:	U.S. Federal Government Document Print Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/4488786

Hidden Bibliographic Details
Other authors / contributors:	Sprinkle, Danny R. Langley Research Center.
Notes:	"June 2001." "Performing organization report number L-18048"--Report documentation page.

Crerar, Lower Level, Bookstacks

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Holdings details from Crerar, Lower Level, Bookstacks
Call Number:	TA357.5.M43L365 2001
c.1	Available Loan period: standard loan Scan and Deliver Request for Pickup Need help? - Ask a Librarian