Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility
By: Kin C. Wong.
Contributors: NASA Glenn Research Center.
Series: NASA/TM -- 2003-212326.; NASA technical memorandum -- 212326.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from the NASA Center for Aerospace Information
Published: 2003
Place of publication: [Cleveland, Ohio]; [Hanover, Md
Language: eng
Format: Microform
Subjects: Axial loads.; Data reduction.; Test facilities.; Thrust measurement.; Exhaust nozzles.; Nozzle geometry.; Calibrating.
Notes: Shipping list no.: 2004-0002-M.

"April 2003."

Also available via Internet from the NASA Technical Report Server web site. Address as of 10/28/04: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20030054464%5F2003060401.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2003?].