Computational Analysis of Fighter Aircraft Wing under Mach Number 0.7 for Small Sweep Angles

Fighter aircraft wings are the leading lift generating components for any aerospace vehicle. The recital of any flying vehicle largely depends on its wing design. Missiles and the fighter aircrafts which are having propulsion system mostly have fins to control and maneuver. In this present paper wor...

Full description

Bibliographic Details

Published in:	Applied Mechanics and Materials Vol. 592-594; no. Dynamics of Machines and Mechanisms, Industrial Research; pp. 1020 - 1024
Main Authors:	Srinivas, G., Potti, Srinivasa Rao
Format:	Journal Article
Language:	English
Published:	Zurich Trans Tech Publications Ltd 15.07.2014
Subjects:	Angles (geometry) Computation Computer simulation Fighter aircraft Flight Guided weapons Wing design Wings (aircraft) CFD Wing Transonic Fighter Aircraft
ISBN:	3038351636, 9783038351634
ISSN:	1660-9336, 1662-7482, 1662-7482
Online Access:	Get full text
Tags:	Add Tag No Tags, Be the first to tag this record!