Library of American University of Madaba
Fundamentals of aerodynamics /
by Anderson, John David.
Series: Anderson series. | McGraw-Hill series in aeronautical and aerospace engineering. Published by : McGraw-Hill, (New York :) Physical details: xxiii, 1106 p. : ill. ; 24 cm. ISBN: 0071289089 Subject(s): Aerodynamics. Year: 2011| Item type | Location | Call Number | Status | Notes | Date Due |
|---|---|---|---|---|---|
 Book |
AUM Main Library English Collections Hall | 629.1323 A545 (Browse Shelf) | Available | JBC/2011/10770 | |
| Book |
AUM Main Library English Collections Hall | 629.1323 A545 (Browse Shelf) | Available | JBC/2011/10770 | |
| Book |
AUM Main Library English Collections Hall | 629.1323 A545 (Browse Shelf) | Available | JBC/2011/10770 | |
| Book |
AUM Main Library English Collections Hall | 629.1323 A545 (Browse Shelf) | Available | JBC/2011/10770 |
Browsing AUM Main Library Shelves, Shelving Location: English Collections Hall Close Shelf Browser
 |
 |
||||||
| 629.04 C456A textbook of transportation engineering / | 629.04 K457Transportation engineering : | 629.04 K457Transportation engineering : | 629.1323 A545Fundamentals of aerodynamics / | 629.1323 A545Fundamentals of aerodynamics / | 629.1323 A545Fundamentals of aerodynamics / |
Includes bibliographical references (p. 1079-1084) and index.
Aerodynamics -- Aerodynamics -- Fundamentals of inviscid, incompressible flow -- Incompressible flow over airfoils -- Incompressible flow over finite wings -- Three-dimensional incompressible flow -- Compressible flow -- Normal shock waves and related topics -- Oblique shock and expansion waves -- Compressible flow through nozzles, diffusers, and wind tunnels -- Subsonic compressible flow over airfoils -- Linearized supersonic flow -- Introduction to numerical techniques for nonlinear supersonic flow -- Elements of hypersonic flow -- Introduction to the fundamental principles and equations of viscous flow -- Special case -- Introduction to boundary layers -- Laminar boundary layers -- Turbulent boundary layers -- Navier-Stokes solutions.
There are no comments for this item.