The book is devoted to calculation methods of a
converging-diverging nozzle used in propulsion and the high
velocity flow. The algorithms and programs given in the book are
intended to help engineers and students to design and calculate the
nozzle parameters to provide optimal parameters for compressible
supersonic flows. The present monograph is a tutorial (handbook) to
calculate and determine the optimal parameters for
converging-diverging nozzles provided supersonic flow. The main
program consists from three main parts: programs for calculation
the profile of the Contraction zone, EOD code for the flow in the
Contraction zone, the program Rott-Crabtree for calculation the
pressure gradient Pohlhausen parameter, the program for the
aerodynamic design of axisymmetric and two-dimensional nozzles for
supersonic and hypersonic wind tunnels, programs for solving
laminar, transitional, or turbulent compressible boundary layer
equations for two-dimensional and axisymmetric flow, and the
program to obtain hypersonic boundary layer stability. The book is
designed to be an instrument for students and scientists interested
in study supersonic flow and high-temperature gas dynamics.
General
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