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...

Celý popis

Podrobná bibliografie

Vydáno v:	Applied Mechanics and Materials Ročník 592-594; číslo Dynamics of Machines and Mechanisms, Industrial Research; s. 1020 - 1024
Hlavní autoři:	Srinivas, G., Potti, Srinivasa Rao
Médium:	Journal Article
Jazyk:	angličtina
Vydáno:	Zurich Trans Tech Publications Ltd 15.07.2014
Témata:	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
On-line přístup:	Získat plný text
Tagy:	Přidat tag Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!