Srivastava, Ashok (1993) Panel methods. In: CFD: Advances and Applications, 1993, India.Full text not available from this repository.
A comprehensive description of panel methods has been given to enable an understanding of the underlying theory and the basic structure of the panel codes for aerodynamic applications. Panel methods have seen peak activity in the industry and remain as yet the sole technique for efficient and practical computations on complex-aircraft configurations. The method of the linearized approach of solving flow problems is well proven and till the turn of the century panel methods will continue to remain as the workhorse for computing aerodynamic characteristics of aircraft shapes in the industry. The alternative Euler and Navier-Stokes solvers have yet to mature for applications to complex shapes, hence panel methods will be in the light for at least another decade.
|Item Type:||Conference or Workshop Item (Paper)|
|Uncontrolled Keywords:||Aerodynamic configurations;Aircraft configurations;Computational fluid dynamics;Panel method (Fluid dynamics);Vortex lattice method;Aerodynamic characteristics;Aerodynamic loads;Computer programs; Stability derivatives|
|Subjects:||AERONAUTICS > Aerodynamics|
|Division/Department:||Computational and Theoretical Fluid Dynamics Division|
|Depositing User:||M/S ICAST NAL|
|Date Deposited:||25 Mar 2008|
|Last Modified:||24 May 2010 09:55|
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