Aerodynamics of Low Reynolds Number Flyers
$44.00 ( ) USD
Part of Cambridge Aerospace Series
- Wei Shyy, University of Michigan, Ann Arbor
- Yongsheng Lian, University of Michigan, Ann Arbor
- Jian Tang, University of Michigan, Ann Arbor
- Dragos Viieru, University of Michigan, Ann Arbor
- Hao Liu, Chiba University, Japan
$44.00 ( )
Adobe eBook Reader
Looking for an examination copy?
If you are interested in the title for your course we can consider offering an examination copy. To register your interest please contact [email protected] providing details of the course you are teaching.
Low Reynolds number aerodynamics is important to a number of natural and man-made flyers. Birds, bats, and insects have been of interest to biologists for years, and active study in the aerospace engineering community, motivated by interest in micro air vehicles (MAVs), has been increasing rapidly. The primary focus of this book is the aerodynamics associated with fixed and flapping wings. The book consider both biological flyers and MAVs, including a summary of the scaling laws-which relate the aerodynamics and flight characteristics to a flyer's sizing on the basis of simple geometric and dynamics analyses, structural flexibility, laminar-turbulent transition, airfoil shapes, and unsteady flapping wing aerodynamics. The interplay between flapping kinematics and key dimensionless parameters such as the Reynolds number, Strouhal number, and reduced frequency is highlighted. The various unsteady lift enhancement mechanisms are also addressed, including leading-edge vortex, rapid pitch-up and rotational circulation, wake capture, and clap-and-fling.Read more
- The focus of this book is on the aerodynamics associated with fixed and flapping wings
- The book considers both biological flyers and MAVs (Micro Air Vehicles), including a summary of the scaling laws
- The various unsteady lift enhancement mechanisms are also addressed, including leading-edge vortex, rapid pitch-up and rotational circulation, wake capture, and clap-and-fling
Reviews & endorsements
"The authors of this book, active pioneers of this new field, have assembled the first comprehensive treatment of the major new aerodynamic aspects pertaining to MAVs...It is well written and illustrated with 29 color and 130 black and white figures. It also has a quite comprehensive reference list. Therefore, it should be of value to scientists and engineers who wish to familiarize themselves with the aerodynamics of birds, insects, and micro air vehicles. In addition, students and anyone else who wishes to learn about the intricacies of aerodynamic lift and thrust generation will bene!t from reading parts of this book."
Max F. Platzer, AIAA Journal
Not yet reviewed
Be the first to review
Review was not posted due to profanity×
- Date Published: February 2009
- format: Adobe eBook Reader
- isbn: 9780511473920
- availability: Adobe Reader ebooks available from eBooks.com
Table of Contents
2. Fixed, rigid wing aerodynamics
3. Flexible wing aerodynamics
4. Flapping wing aerodynamics.
Welcome to the resources site
Here you will find free-of-charge online materials to accompany this book. The range of materials we provide across our academic and higher education titles are an integral part of the book package whether you are a student, instructor, researcher or professional.
Find resources associated with this titleYour search for '' returned .
Type Name Unlocked * Format Size
*This title has one or more locked files and access is given only to instructors adopting the textbook for their class. We need to enforce this strictly so that solutions are not made available to students. To gain access to locked resources you either need first to sign in or register for an account.
These resources are provided free of charge by Cambridge University Press with permission of the author of the corresponding work, but are subject to copyright. You are permitted to view, print and download these resources for your own personal use only, provided any copyright lines on the resources are not removed or altered in any way. Any other use, including but not limited to distribution of the resources in modified form, or via electronic or other media, is strictly prohibited unless you have permission from the author of the corresponding work and provided you give appropriate acknowledgement of the source.
If you are having problems accessing these resources please email [email protected]
Sorry, this resource is locked
Please register or sign in to request access. If you are having problems accessing these resources please email [email protected]Register Sign in
You are now leaving the Cambridge University Press website. Your eBook purchase and download will be completed by our partner www.ebooks.com. Please see the permission section of the www.ebooks.com catalogue page for details of the print & copy limits on our eBooks.Continue ×