Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility /

Bibliographic Details

Main Author:	Wong, Kin C.
Corporate Author:	NASA Glenn Research Center
Format:	Government Document Microform Book
Language:	English
Published:	[Cleveland, Ohio] : [Hanover, Md.] : National Aeronautics and Space Administration, Glenn Research Center ; [Available from the NASA Center for Aerospace Information], [2003]
Series:	NASA technical memorandum ; 212326.
Subjects:	Axial loads. Data reduction. Test facilities. Thrust measurement. Exhaust nozzles. Nozzle geometry. Calibrating. Testing laboratories.
Online Access:	https://purl.fdlp.gov/GPO/LPS55251