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An experimental investigation of gapwise periodicity and unsteady aerodynamic response in an oscillating cascade. Volume 2: Data report. Part 2: Mode 2 dataComputer data are provided for tests conducted on a linear cascade of airfoils oscillating in pitch to measure the unsteady pressure response on selected blades along the leading edge plane of the cascade, over the chord of the center blade, and on the sidewall in the plane of the leading edge.
Document ID
19820010307
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Carta, F. O. (United Technologies Research Center East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-165457-VOL-2-PT-2
Accession Number
82N18181
Funding Number(s)
CONTRACT_GRANT: NAS2-22018
PROJECT: RTOP 510-55-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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