A good understanding of turbulent compressible flows is
essential to the design and operation of high-speed vehicles. Such
flows occur, for example, in the external flow over the surfaces of
supersonic aircraft, and in the internal flow through the engines.
Our ability to predict the aerodynamic lift, drag, propulsion and
maneuverability of high-speed vehicles is crucially dependent on
our knowledge of turbulent shear layers, and our understanding of
their behavior in the presence of shock waves and regions of
changing pressure. Turbulent Shear Layers in Supersonic Flow
provides a comprehensive introduction to the field, and helps
provide a basis for future work in this area. Wherever possible we
use the available experimental work, and the results from numerical
simulations to illustrate and develop a physical understanding of
turbulent compressible flows.
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