Calculation of nonequilibrium hypersonic turbulent boundary layers and comparisons with experimental data-Reference-Cited by-同舟云学术

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Calculation of nonequilibrium hypersonic turbulent boundary layers and comparisons with experimental data

Published:1970-08 Issue:8 Volume:8 Page:1462-1469
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

BUSHNELL DENNIS M.¹,BECKWITH IVAN E.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.5924

Reference36 articles.

1. Bradshaw, P. and Ferriss, D. H. "Calculation of Boundary-Layer Development Using the Turbulent Energy Equation. II-Compressible Flow on Adiabatic Walls," NPL Aero Report 1217, Nov.24,1966, National Physical Lab., Aerodynamics Div., Teddington,England.

2. On Turbulent Flow Near a Wall

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