Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation /

Bibliographic Details
Main Author:	Kniskern, Marc W.
Corporate Authors:	United States. National Aeronautics and Space Administration, North Carolina State University. Department of Mechanical and Aerospace Engineering
Format:	Government Document Book
Language:	English
Published:	Raleigh, [N.C.] : North Carolina State University, Dept. of Mechanical and Aerospace Engineering, 1990.
Series:	NASA contractor report ; NASA CR-186585.
Subjects:	Exhaust flow simulation. Force distribution. Gas injection. Strain gage balances. Temperature effects. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/LPS69058

Description
Item Description:	Shipping list number: 1990-0881-M. Distributed to depository libraries in microfiche. Microform.
Physical Description:	1 volume Also available via Internet from the NTRS web site. Address as of 4/19/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900012459%5F1990012459.pdf; current access is available via PURL.
Bibliography:	Includes bibliographical references.