Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation.

Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. Part III, Computer program manual / by J. Schneider and J. Boccio.

A computer program is described capable of determining the properties of a compressible turbulent boundary layer with pressure gradient and heat transfer. The program treats the two-dimensional problem assuming perfect gas and Crocco integral energy solution. A compressibility transformation is appl...

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Bibliographic Details
Online Access: Search for the full-text version of this title in HathiTrust
Main Author: Schneider, J.
Corporate Authors: General Applied Science Laboratories (Westbury, Nassau County, N.Y.), Langley Research Center, United States. National Aeronautics and Space Administration
Other Authors: Boccio, J.
Format: Government Document Book
Language:English
Published: Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor], 1972.
Series:NASA contractor report ; NASA CR-1925.
Subjects:
Heat > Transmission.
Turbulent boundary layer.
Boundary layer.
Computer programs.
Heat transfer.
Pressure gradients.
Boundary layer flow.
Compressible boundary layer.
Conservation equations.
Crocco method.

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Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number: NAS 1.26:1925
NAS 1.26:1925 Available Place a Hold

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