RANS computations for flow through a variable mach number flexible nozzle at mach 4

Dutta, Vimala and Dutta, PK and Sajjan, Sharanappa V (2008) RANS computations for flow through a variable mach number flexible nozzle at mach 4. In: Proceedings of the International Conference on Aerospace Science and Technology, 26-28 Jun 2008, Bangalore, India.

[img] PDF
CF7.pdf
Restricted to Registered users only

Download (216kB)

Abstract

Numerical simulation of flow through a Variable Mach number Flexible Nozzle (VMFN) at Mach 4 is carried out using the CFD code IMPRANS to validate the design of the nozzle based on the method of characteristics with boundary layer correction. The CFD analysis for the contour uses an implicit Reynolds-averaged Navier-Stokes (RANS) solver with Baldwin-Lomax turbulence model. Detailed flow characteristics like the centerline Mach number distribution and Mach contours of the steady flow through the converging x2013; diverging nozzle are obtained to study and assess the suitability of the design

Item Type: Conference or Workshop Item (Paper)
Uncontrolled Keywords: Baldwin-Lomax turbulence model;Variable mach number flexible nozzle (VMFN)
Subjects: AERONAUTICS > Aeronautics (General)
Depositing User: Users 11 not found.
Date Deposited: 06 Apr 2010
Last Modified: 17 Jun 2010 09:56
URI: http://nal-ir.nal.res.in/id/eprint/5274

Actions (login required)

View Item View Item