by: John M. Seddon, Simon Newman
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97067bc6bc6b3e9664c6c9b49ed8cf3a
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15.75 MB
[ 16512587 bytes ]
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| type:
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.pdf
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| status:
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normal
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| language:
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en [ english ]
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| submitted by:
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anonymous
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| 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 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 practising engineers looking for an introduction to or
refresher course on the subject. |
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