Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /

Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /

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Bibliographic Details
Author / Creator:	Schuster, D. M. (David M.)
Imprint:	Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, 2001.
Description:	37 p. : ill. ; 28 cm.
Language:	English
Series:	NASA TM- ; 2001-210828 NASA technical memorandum ; 2001-210828.
Subject:	Plates (Engineering) Transonic wind tunnels. Unsteady flow (Aerodynamics) Plates (Engineering) Transonic wind tunnels. Unsteady flow (Aerodynamics)
Format:	U.S. Federal Government Document Print Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/4442964

Hidden Bibliographic Details
Other authors / contributors:	Langley Research Center.
Notes:	"March 2001." "Performing organization report number L-18054"--Report documentation page.

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Call Number:	TL567.W5S387 2001
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