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Calhoun, Institutional Archive of the Naval Postgraduate School
Thesis . 1987
Data sources: Calhoun, Institutional Archive of the Naval Postgraduate School
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High Reynolds number

descriptionPublicationkeyboard_double_arrow_right Thesis 01 Dec 1987 English
Authors: Cowles, Lisa J.;

High Reynolds number

Abstract

A Navier-Stokes code, developed by N.L. Sankar, and an Interactive Boundary Layer code, developed by Tuncer Cebeci, are implemented for high Reynolds number, low Mach flows over a NACA 0012 airfoil. Upper surface pressure distributions, coefficients of lift, coefficients of friction, and velocity profiles obtained from the Navier-Stokes code are compared to results obtained from the Cebeci Interactive Boundary Layer code for steady flow. The steady state cases investigated aaare at .3 Mach and a Reynolds number of 1.3 million. Approved for public release; distribution is unlimited. Civilian, United States Navy http://archive.org/details/highreynoldsnumb1094522825

Keywords

Pressure coefficient, Navier-Stokes, Skin friction coefficient, Aeronautics, Interactive Boundary Layer theory, Lift coefficient, Velocity profiles

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selected citations
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
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