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Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications (Progress in Astronautics and Aeronautics)

Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications (Progress in Astronautics and Aeronautics)

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Creators: Thomas J. Mueller, American Institute Of Aeronautics And Astronautics
Publisher: AIAA (American Institute of Aeronautics & Ast
Category: Book

List Price: $119.95
Buy New: $95.96
You Save: $23.99 (20%)



New (9) from $95.96

Avg. Customer Rating: 5.0 out of 5 stars 1 reviews
Sales Rank: 886693

Media: Hardcover
Number Of Items: 1
Pages: 586
Shipping Weight (lbs): 2.2
Dimensions (in): 9.2 x 6.3 x 1.5

ISBN: 1563475170
EAN: 9781563475177
ASIN: 1563475170

Publication Date: February 1, 2002
Shipping: Eligible for Super Saver Shipping
Promotion: Save $10.00 when you spend $50.00 or more on Qualifying Items offered by Amazon.com. Enter code BMLSAVES at checkout. Terms and Conditions
Availability: In stock soon. Order now to get in line. First come, first served.

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Editorial Reviews:

Product Description
Recently, there has been a serious effort to design aircraft that are as small as possible for special, limited-duration missions. These vehicles may carry visual, acoustic, chemical, or biological sensors for such missions as traffic management, hostage situation surveillance, rescue operations, etc. The goal is to develop aircraft systems that weigh less than 90 grams, with a 15-centimetre wingspan. Since it is not possible to meet all of the design requirements of a micro air vehicle with current technology, research is proceeding. This new book reports on the latest research in the area of aerodynamic efficiency of various fixed-wing, flapping wing, and rotary wing concepts. It presents the progress made by over 50 active researchers in the field from Canada, Europe, Japan, and the United States. It is the only book of its kind.


Customer Reviews:

5 out of 5 stars Helpful for MAV Design   February 16, 2003
 2 out of 2 found this review helpful

I found this book extremely helpful for information while recently working on my senior design project at the Rochester Institute of Technology. As of winter 2002/2003 there is very little liable information on micro air vehicle aerodynamics available free through technical papers and other readings that I could find. After looking for information for nearly a month I purchased this book and had several of my questions on MAV design and applications answered. This book is primarily a collection of AIAA and university MAV technical papers. I would recommend this book to any college student or professor working on a MAV related project.

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