"The book is designed to better support and cover compressible flow material in gas turbine and aerodynamics courses. It begins with a brief review of thermodynamics and control volume fluid dynamics, then proceeds to cover isentropic flow, normal shock waves, shock tubes, oblique shock waves, Prandtl-Meyer expansion fans, Fanno-line flow, Rayleigh-line flow, and conical shock waves. The book includes a chapter on linearized flow following chapters on oblique shocks and Prandtl-Meyer flows to appropriately ground students in this approximate method. It includes detailed appendices to support problem solutions and covers new oblique shock tables, which allow for quick and accurate solutions of flows with concave corners. The book is intended for senior undergraduate engineering students studying thermal-fluids and practicing engineers in the areas of aerospace or energy conversion"--
TOPICAL NAME USED AS SUBJECT
Entry Element
Gas dynamics.
Entry Element
Gas flow.
Entry Element
Shock waves.
Entry Element
Compressibility.
DEWEY DECIMAL CLASSIFICATION
Edition
23
LIBRARY OF CONGRESS CLASSIFICATION
Class number
QC168
Book number
.
A44
2021
PERSONAL NAME - PRIMARY RESPONSIBILITY
Entry Element
Ames, Forrest E.,
PERSONAL NAME - ALTERNATIVE RESPONSIBILITY
Tang, Clement,
ORIGINATING SOURCE
Country
ایران
Agency
University of Tehran. Library of College of Science