Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications

Author:   Thomas J. Mueller
Publisher:   American Institute of Aeronautics & Astronautics
Volume:   v. 195
ISBN:  

9781563475177


Pages:   650
Publication Date:   31 January 2002
Format:   Hardback
Availability:   In Print   Availability explained
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Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications


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Overview

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.

Full Product Details

Author:   Thomas J. Mueller
Publisher:   American Institute of Aeronautics & Astronautics
Imprint:   American Institute of Aeronautics & Astronautics
Volume:   v. 195
Dimensions:   Width: 16.10cm , Height: 3.70cm , Length: 23.00cm
Weight:   0.998kg
ISBN:  

9781563475177


ISBN 10:   1563475170
Pages:   650
Publication Date:   31 January 2002
Audience:   College/higher education ,  Professional and scholarly ,  Undergraduate ,  Postgraduate, Research & Scholarly
Format:   Hardback
Publisher's Status:   Active
Availability:   In Print   Availability explained
This item will be ordered in for you from one of our suppliers. Upon receipt, we will promptly dispatch it out to you. For in store availability, please contact us.

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