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Experimental study of flow due to an isolated suction hole and a partially plugged suction slotDetails for construction of a model of a partially plugged, laminar flow control, suction slot and an isolated hole are presented. The experimental wind tunnel facility and instrumentation is described. Preliminary boundary layer velocity profiles (without suction model) are presented and shown to be in good agreement with the Blasius laminar profile. Recommendations for the completion of the study are made. An experimental program for study of transition on a rotating disk is described along with preliminary disturbance amplification rate data.
Document ID
19800010070
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Goglia, G. L. (Old Dominion Univ. Norfolk, VA, United States)
Wilkinson, S. P. (Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1980
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-162808
Report Number: NASA-CR-162808
Accession Number
80N18340
Funding Number(s)
CONTRACT_GRANT: NSG-1491
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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