Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number /

Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number / by Eli Reshotko and Ivan E. Beckwith.

The equations for development of the compressible laminar boundary layer over a yawed infinite cylinder are presented. For compressible flow with a pressure gradient the chordwise and spanwise flows are not independent. By use of the Stewartson transformation and a linear viscosity-temperature relat...

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Bibliographic Details
Main Author: Reshotko, Eli
Corporate Authors: Lewis Flight Propulsion Laboratory, Langley Aeronautical Laboratory, United States. National Advisory Committee for Aeronautics
Other Authors: Beckwith, Ivan E.
Format: Government Document Book
Language:English
Published: Washington : National Advisory Committee for Aeronautics, [1957]
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3986.
Subjects:
Laminar flow > Mathematical models.
Boundary layer > Mathematical models.
Compressibility > Mathematical models.
Yawing (Aerodynamics) > Mathematical models.
Heat > Transmission > Mathematical models.
Leading edges (Aerodynamics) > Mathematical models.
Cylinders > Mathematical models.

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Call Number: Y 3.N 21/5:6/3986
Y 3.N 21/5:6/3986 Available Place a Hold

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