Langley 16-ft. Transonic Tunnel Pressure Sensitive Paint System

Langley 16-ft. Transonic Tunnel Pressure Sensitive Paint System [microform] / Danny R. Sprinkle ... [and others]

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Bibliographic Details
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Corporate Author:	Langley Research Center
Other Authors:	Sprinkle, Danny R.
Other title:	Langley Sixteen Foot Transonic Tunnel Pressure Sensitive Paint System.
Format:	Government Document Microfilm Book
Language:	English
Published:	Hampton, Va. : Hanover MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information (CASI), [2001]
Series:	NASA technical memorandum ; 211017.
Subjects:	Transonic wind tunnels. Pressure sensitive paints. Pressure measurement. Flow visualization.

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Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:211017
NAS 1.15:211017	Restricted Place a Hold

Online

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Call Number:	NAS 1.15:211017
NAS 1.15:211017	Available