Somashekar V., Sarat Maharana

Broschiertes Buch

Micro Aerial Vehicle

Unsteady Aerodynamics, Low Reynolds Number

Beschreibung

A bird or insect sized flapping wing Micro Aerial Vehicle (MAV) whose wingspan is of the order of a few centimeters cannot be physically built or flown today; they can be designed, tested, flown and studied on the computer using numerical simulation technique. While finalizing a design is quite significant in case of MAV, understanding the flow field environment in which MAVs fly is equally a requirement. The flow field environments encountered by Micro Air Vehicles are fundamentally unsteady - whether for fixed-wing, rotary-wing or flapping-wing configurations. High lift generation is typically a result of unsteady fluid flow phenomena in flapping flight of small birds and insects. Along with a good understanding of flow field environment of an MAV the insight into the aerodynamics characteristics of it calls for an investigation. These characteristics greatly influence the design of a prototype of an MAV which can serve the purpose of a specific application. As a first step towards exploring the flow environment and computing the aerodynamic characteristics of a smaller MAV we have chosen a fixed wing MAV for which a study is attempted considering a three dimensional flow field.

Autor

Mr. SOMASHEKAR V, a well-known Asst. Professor and researcher. He has a mixed experience of industry as well as teaching in the area of Mechanical and Aeronautical Engineering. He has published several research papers in national & international Journals and conferences. His Areas of research interest includes: Aerodynamics, CFD, Heat Transfer, FM.

Produktdetails

• Verlag: LAP Lambert Academic Publishing
• Seitenzahl: 136
• Erscheinungstermin: 20. Februar 2014
• Englisch
• Abmessung: 220mm x 150mm x 9mm
• Gewicht: 197g
• ISBN-13: 9783659143878
• ISBN-10: 3659143871
• Artikelnr.: 40532881