Analytical Model Of Rotor Wake Aerodynamics In Ground Effect
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Free Wake Analysis of Hover Performance Using a New Influence Coefficient Method
Author | : Todd R. Quackenbush |
Publisher | : |
Total Pages | : 108 |
Release | : 1990 |
Genre | : Rotors (Helicopters) |
ISBN | : |
Monthly Catalog of United States Government Publications
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : |
Release | : 1985 |
Genre | : Government publications |
ISBN | : |
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index
Bramwell's Helicopter Dynamics
Author | : A. R. S. Bramwell |
Publisher | : Elsevier |
Total Pages | : 403 |
Release | : 2001-04-06 |
Genre | : Technology & Engineering |
ISBN | : 0080528309 |
Since the original publication of 'Bramwell's Helicopter Dynamics' in 1976, this book has become the definitive text on helicopter dynamics and a fundamental part of the study of the behaviour of helicopters. This new edition builds on the strengths of the original and hence the approach of the first edition is retained. The authors provide a comprehensive overview of helicopter aerodynamics, stability, control, structural dynamics, vibration, aeroelastic and aeromechanical stability. As such, Bramwell's Helicopter Dynamics is essential for all those in aeronautical engineering.THE single volume comprehensive guide for anyone working with helicopters Written by leading worldwide experts in the field
Principles of Helicopter Aerodynamics with CD Extra
Author | : Gordon J. Leishman |
Publisher | : Cambridge University Press |
Total Pages | : 860 |
Release | : 2006-04-24 |
Genre | : Science |
ISBN | : 9780521858601 |
Written by an internationally recognized teacher and researcher, this book provides a thorough, modern treatment of the aerodynamic principles of helicopters and other rotating-wing vertical lift aircraft such as tilt rotors and autogiros. The text begins with a unique technical history of helicopter flight, and then covers basic methods of rotor aerodynamic analysis, and related issues associated with the performance of the helicopter and its aerodynamic design. It goes on to cover more advanced topics in helicopter aerodynamics, including airfoil flows, unsteady aerodynamics, dynamic stall, and rotor wakes, and rotor-airframe aerodynamic interactions, with final chapters on autogiros and advanced methods of helicopter aerodynamic analysis. Extensively illustrated throughout, each chapter includes a set of homework problems. Advanced undergraduate and graduate students, practising engineers, and researchers will welcome this thoroughly revised and updated text on rotating-wing aerodynamics.
Basic Helicopter Aerodynamics
Author | : John M. Seddon |
Publisher | : John Wiley & Sons |
Total Pages | : 292 |
Release | : 2011-06-09 |
Genre | : Technology & Engineering |
ISBN | : 1119972728 |
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 MATLABĀ® 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.