Numerical investigations of small-amplitude disturbances in a boundary layer with impinging shock wave at Ma=4.8-Reference-Cited by-同舟云学术

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Numerical investigations of small-amplitude disturbances in a boundary layer with impinging shock wave at Ma=4.8

Published:2002 Issue:7 Volume:14 Page:2088
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Phys. Fluids

Author:

Pagella Alessandro,Rist Ulrich,Wagner Siegfried

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Reference23 articles.

1. W. Saric, E. Reshotko, and D. Arnal, “Hypersonic laminar-turbulent transition,” AGARD AR-319 (1998).

2. L. Mack, “Boundary layer stability theory,” Jet Propulsion Laboratory, Pasadena, Tech. Rep. 900-277 (1969).

3. L. Lees and C. Lin, “Investigation of the compressible laminar boundary layer,” NACA Tech. Note 1115 (1946).

4. J. Ackeret, F. Feldmann, and N. Rott, Report no. 10, ETH Zürich, Institut für Aerodynamik, 1946.

5. The Interaction Between Boundary Layer and Shock Waves in Transonic Flow

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