Calculation of vortex flow on a delta wing

Kumar, A and Sudharsan, R (1993) Calculation of vortex flow on a delta wing. Technical Report. National Aerospace Laboratories, Bangalore, India.

[img] PDF
tr_pdcf_9324_R86266_txt.pdf
Restricted to Repository staff only

Download (3MB)

Abstract

Solutions of Eul er equations for flow over a sharp leading-edge delta wing are presented for angles of incidence upto 46 degree using a conventional H-0 grid and a multi-block grid consisting of an inner block of conical grid covered by an outer block of H-0 grid, and computed solutions on two grids are compared . The multi -block grid i s expected to provide a better resolution of the vorti cal flow near the apex due to conical nature of the surrounding grid .

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Euler equations;Multi-block grid
Subjects: ENGINEERING > Fluid Mechanics and Thermodynamics
ASTRONAUTICS > Astrodynamics
Depositing User: Users 49 not found.
Date Deposited: 10 Jul 2006
Last Modified: 24 May 2010 04:13
URI: http://nal-ir.nal.res.in/id/eprint/1651

Actions (login required)

View Item View Item