NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Friction factor data for flat plate tests of smooth and honeycomb surfacesFriction factors for honeycomb surfaces were measured with a flat plate tester. The flat plate test apparatus was described and a method was discussed for determining the friction factor experimentally. The friction factor model was developed for the flat plate test based on the Fanno Line Flow. The comparisons of the friction factor were plotted for smooth surfaces and six-honeycomb surfaces with three-clearances, 6.9 bar to 17.9 bar range of inlet pressures, and 5,000 to 100,000 range of the Reynolds number. The optimum geometries for the maximum friction factor were found as a function of cell width to cell depth and cell width to clearance ratios.
Document ID
19890014505
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Ha, Tae Woong
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1989
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.26:184977
TL-SEAL-1-89
NASA-CR-184977
Report Number: NAS 1.26:184977
Report Number: TL-SEAL-1-89
Report Number: NASA-CR-184977
Accession Number
89N23876
Funding Number(s)
CONTRACT_GRANT: NAG3-181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available