Numerical simulation of a flow around airfoil using inviscid gas equations

dc.contributor.author	Terekhin A.A.	en
dc.contributor.author	Sidel'nikov R.V.	en
dc.contributor.author	Pavluyk Yu.S.	en
dc.date.accessioned	2018-10-16T06:53:44Z
dc.date.available	2018-10-16T06:53:44Z
dc.date.issued	2009
dc.identifier.issn	10687998
dc.identifier.uri	http://dspace.susu.ru/handle/0001.74/20612
dc.description.abstract	A method for determining a field of inviscid gas equation application in finding the aerodynamic characteristics of bodies is proposed; as an example, use is made of airfoils for which extensive experimental data are available. The comparative analysis of physical and numerical simulation results showed a good verification of the method presented. © Allerton Press, Inc., 2009.	en]
dc.language.iso	English
dc.relation.ispartof	Russian Aeronautics	en]
dc.subject	Aerodynamic characteristics	en]
dc.subject	Comparative analysis	en]
dc.subject	Experimental datum	en]
dc.subject	Inviscid gas	en]
dc.subject	Numerical simulations	en]
dc.subject	Computer simulation	en]
dc.subject	Flow simulation	en]
dc.subject	Gas dynamics	en]
dc.subject	Airfoils	en]
dc.title	Numerical simulation of a flow around airfoil using inviscid gas equations	en
dc.type	Article	en]
dc.identifier.doi	10.3103/S1068799809010206
dc.identifier.scopus	https://www.scopus.com/inward/record.uri?eid=2-s2.0-65549141862&doi=10.3103%2fS1068799809010206&partnerID=40&md5=9b855bd4f1eb4b6d33df5dc62cf61aee