Holographic Analysis of ParticleInduced Hypersonic Bow-Shock Distortions

Author:

Hove D. T.1,Smith A. A.1

Affiliation:

1. Science Applications, Inc., El Segundo, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference15 articles.

1. Model Equations for Turbulent Shear Flow

2. Turbulence-Model Predictions for Turbulent Boundary Layers

3. A model for inhomogeneous turbulent flow

4. Knight, D. D. "An Analytical Investigation of Turbulent Flow Over a Wavy Boundary," Ph.D. thesis,1974, Department of Aeronautics, California Instituteof Technology, Pasadena, Calif.

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