Optimized construction of a composite MAV wing using CFD analysis

Thulasi Durai, D and Viswamurthy , SR and Byji, Varughese and Dayananda, GN and Subrahmanya, MB and Kulkarni, DS and Rajani, BN and Mathur, JS (2009) Optimized construction of a composite MAV wing using CFD analysis. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2009), 10-12 December 2009, Bangalore.

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The development of a rigid yet light-weight composite MAV wing is presented in this work. A grid based construction was opted for the fabrication of the wing. The distribution of the grids, their size and the number of composite plies were arrived based on a finite element based structural analysis of the wing. The aerodynamic loads acting on the wing structure were estimated using CFD simulations. The CFD computations were carried out using a multi-block structured RANS code based on an implicit finite volume algorithm to solve the time averaged Navier-Stokes equation. Based on the computational results, two light-weight MAV wings were fabricated having very high flexural stiffness. One was based on a sandwich type construction and the other was a planar grid construction.

Item Type: Conference or Workshop Item (Paper)
Subjects: AERONAUTICS > Aerodynamics
AERONAUTICS > Aircraft Design, Testing & Performance
Depositing User: Dr. Viswamurthy S R
Date Deposited: 12 Jul 2010 04:28
Last Modified: 12 Jul 2010 04:28
URI: http://nal-ir.nal.res.in/id/eprint/8575

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