CLCV21
LanguageENG
PublishYear2017
publishCompany
McGraw Hill
EISBN
9789388028301
PISBN
9789388028295
edition
1
- Product Details
- Contents
This book is developed to serve as a concise text for a course on helicopter aerodynamics at the introductory level. It introduces to the rotary-wing aerodynamics, with applications to helicopters, and application of the relevant principles to the aerodynamic design of a helicopter rotor and its blades. The basic aim of this book is to make a complete text covering both the basic and applied aspects of theory of rotary-wing flying machine for students, engineers, and applied physicists. Considerable number of solved examples and exercise problems with answers are coined for this book.
SALIENT FEATURES
To provide an introductory treatment of the aerodynamic theory of rotary-wing aircraft
To study the fundamentals of rotor aerodynamics for rotorcraft in hovering flight, axial flight, and forward flight modes
To perform blade element analysis, investigate rotating blade motion, and quantify basic helicopter performance
TARGET AUDIENCE
BE/B.Tech (Aeronautical/Aerospace Engineering)