Euler Simulation of NCA-F90-D-OV-112 Aircraft Configuration

Singh, Manish K and Madhu Babu, K and Dhanalakshmi, K and Mathur, J. S. (2012) Euler Simulation of NCA-F90-D-OV-112 Aircraft Configuration. Project Report. CSIR-NAL, Bangalore.

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Abstract

Euler simulations are carried out for NCA-F90-D-OV-112 aircraft at Mach number of 0.7 with angle of attack varying from -4 to 7 using JUEL3D Euler solver which is based on the Jameson JST scheme. For this purpose a structured grids consisting of 180 blocks with approximately 45 Million grid cells are created. In absence of any experimental data, the present computations are compared with computations from another Euler solver called ‘Hyena’. The computational data obtained from both solvers are in good agreement with each other.

Item Type: Proj.Doc/Technical Report (Project Report)
Uncontrolled Keywords: NCA, Euler Solution
Subjects: AERONAUTICS > Aerodynamics
AERONAUTICS > Aircraft Design, Testing & Performance
Division/Department: Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division
Depositing User: Mr Manish K Singh
Date Deposited: 21 Sep 2012 13:54
Last Modified: 21 Sep 2012 13:54
URI: http://nal-ir.nal.res.in/id/eprint/10942

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