Overview:
Basic Helicopter Aerodynamics is widely appreciated as an
easily accessible, rounded introduction to the first principles of the
aerodynamics of helicopter flight. Simon Newman has brought this third edition
completely up to date with a full new set of illustrations and imagery. An
accompanying website www.wiley.com/go/seddon contains all the calculation files
used in the book, problems, solutions, PPT slides and supporting MATLAB® code.
Simon Newman addresses the unique considerations applicable
to rotor UAVs and MAVs, and coverage of blade dynamics is expanded to include
both flapping, lagging and ground resonance. New material is included on blade
tip design, flow characteristics surrounding the rotor in forward flight, tail
rotors, brown-out, blade sailing and shipborne operations.
Concentrating on the well-known Sikorsky configuration of
single main rotor with tail rotor, early chapters deal with the aerodynamics of
the rotor in hover, vertical flight, forward flight and climb. Analysis of
these motions is developed to the stage of obtaining the principal results for
thrust, power and associated quantities. Later chapters turn to the
characteristics of the overall helicopter, its performance, stability and
control, and the important field of aerodynamic research is discussed, with
some reference also to aerodynamic design practice.
This introductory level treatment to the aerodynamics of
helicopter flight will appeal to aircraft design engineers and undergraduate
and graduate students in aircraft design, as well as practicing engineers
looking for an introduction to or refresher course on the subject.
Download:
I Can't download any of the books..!!
ReplyDeleteGot a message "Warning: mysql_close() expects parameter 1 to be resource, null given in /home/pdfbook1/public_html/download_manager.php on line 245
Warning: Cannot modify header information - headers already sent by (output started at /home/pdfbook1/public_html/download_manager.php:245) in /home/pdfbook1/public_html/download_manager.php on line 246"