Computation of 3-D Transonic Flow for Wings and Wing Body13; Configuration

Chakrabartty, SK and Subramanian, NR and Siddalingappa, SR and Das, AK (1987) Computation of 3-D Transonic Flow for Wings and Wing Body13; Configuration. Technical Report. National Aeronautical Laboratory, Bangalore, India.

[img] PDF
tr_pd_fm_8707_R69174_txt.pdf
Restricted to Repository staff only

Download (1MB)

Abstract

The object of this report is to summarize the work done on 3D transonic flow computations during the year 1986-87. Attempts were made to generate 0 type grids for the fuselage to match with the 0 grids for the wing. In addition a 3D Euler code for wings was developed and applied to several wing configurations ranging from large to moderate aspect ratio. Typical results for a rectangular wing (Aspect ratio of Mv = 0.75 J =2x2019;, as well as cropped delta wing are provided. Comparison with STWING, SFL022 and experiments are made.

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Transonic flows;Wings
Subjects: ENGINEERING > Fluid Mechanics and Thermodynamics
Depositing User: Users 11 not found.
Date Deposited: 02 May 2006
Last Modified: 24 May 2010 04:10
URI: http://nal-ir.nal.res.in/id/eprint/1176

Actions (login required)

View Item View Item