Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation
By: by Marc W. Kniskern.
Contributors: United States. National Aeronautics and Space Administration.; North Carolina State University. Dept. of Mechanical and Aerospace Engineering.
Series: NASA contractor report -- NASA CR-186585.
Publisher: North Carolina State University, Dept. of Mechanical and Aerospace Engineering
Published: 1990
Place of publication: Raleigh, [N.C.]
Language: eng
Format: Microform
Subjects: Exhaust flow simulation.; Force distribution.; Gas injection.; Strain gage balances.; Temperature effects.; Wind tunnel tests.
Notes: Shipping list no.: 1990-0881-M.

Distributed to depository libraries in microfiche.

Includes bibliographical references.

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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1990. 1 microfiche.