Aerodynamics of delta wing-body Combinations at high angles of attack - A project proposal

Viswanath , PR (1985) Aerodynamics of delta wing-body Combinations at high angles of attack - A project proposal. Project Report. National Aerospace Laboratories, Bangalore.

[img] PDF
PD_AE_8518.pdf

Download (64kB)

Abstract

Aerodynamics of highly swept wing-body configurations are dominated by vortex flows at high angles of attack . This research is proposed with a view to improving our general understanding on the nature of the vortical interactions on delta wing-body combinations and to provide information on static aerodynamic characteristics at high angles of attack. Experiments are proposed on two delta wing-body configurations at subsonic speeds. It is hoped that the results obtained from this investigation will be useful in the preliminary design of combat aircraft of the future.

Item Type: Monograph (Project Report)
Uncontrolled Keywords: High angle of attack aerodynamics;Delta wings
Subjects: AERONAUTICS > Aerodynamics
Depositing User: Smt Bhagya Rekha KA
Date Deposited: 26 Sep 2012 08:39
Last Modified: 26 Sep 2012 08:39
URI: http://nal-ir.nal.res.in/id/eprint/11024

Actions (login required)

View Item View Item