NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Exact Calculation of Laminar Boundary Layer in Longitudinal Flow over a Flat Plate with Homogeneous SuctionLately it has been proposed to reduce the friction drag of a body in a flow for the technically important large Reynolds numbers by the following expedient: the boundary layer, normally turbulent, is artificially kept laminar up to high Reynolds numbers by suction. The reduction in friction drag thus obtained is of the order of magnitude of 60 to 80 percent of the turbulent friction drag, since the latter, for large Reynolds numbers, is several times the laminar friction drag. In considering the idea mentioned one has first to consider whether suction is a possible means of keeping the boundary layer laminar. This question can be answered by a theoretical investigation of the stability of the laminar boundary layer with suction. A knowledge, as accurate as possible, of the velocity distribution in the laminar boundary layer with suction forms the starting point for the stability investigation. E. Schlichting recently gave a survey of the present state of calculation of the laminar boundary layer with suction.
Document ID
20050019547
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Iglisch, Rudolf
(National Advisory Committee for Aeronautics Washington, DC, United States)
Date Acquired
August 22, 2013
Publication Date
April 1, 1949
Publication Information
Publication: Schriften der Deutschen Akademie der Luftfahrtforschung
Volume: 8
Issue: 1
Subject Category
Aerodynamics
Report/Patent Number
NACA-TM-1205
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available