The Shock Tube as a Short Duration Wind Tunnel

KAMIMOTO, Gorō; SHIMIZU, Takashi; AKAMATSU, Teruaki

ダウンロード数: 21

http://hdl.handle.net/2433/280414

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DCフィールド	値	言語
dc.contributor.author	KAMIMOTO, Gorō	en
dc.contributor.author	SHIMIZU, Takashi	en
dc.contributor.author	AKAMATSU, Teruaki	en
dc.date.accessioned	2023-03-28T09:05:23Z	-
dc.date.available	2023-03-28T09:05:23Z	-
dc.date.issued	1958-08-15	-
dc.identifier.uri	http://hdl.handle.net/2433/280414	-
dc.description.abstract	Descriptions of the shock tube recently constructed at Aerodynamic Laboratory and of some experimental results obtained thereby are given in this paper. The shock tube has a cross section of 156mm high and 50mm wide and is 3370mm long. By this shock tube a uniform flow field, free from turbulence, is obtained and its Mach number may freely be adjusted from zero to the supersonic range. Instantaneous photographs of the flow patterns have been taken by using the Mach-Zehnder interferometer or the schlieren method and are shown in this paper.	en
dc.language.iso	eng	-
dc.publisher	Faculty of Engineering, Kyoto University	en
dc.publisher.alternative	京都大学工学部	ja
dc.subject.ndc	500	-
dc.title	The Shock Tube as a Short Duration Wind Tunnel	en
dc.type	departmental bulletin paper	-
dc.type.niitype	Departmental Bulletin Paper	-
dc.identifier.ncid	AA00732503	-
dc.identifier.jtitle	Memoirs of the Faculty of Engineering, Kyoto University	en
dc.identifier.volume	20	-
dc.identifier.issue	3	-
dc.identifier.spage	163	-
dc.identifier.epage	181	-
dc.textversion	publisher	-
dc.sortkey	04	-
dc.address	Department of Mechanical Engineering	en
dc.address	Department of Mechanical Engineering	en
dc.address	Department of Mechanical Engineering	en
dcterms.accessRights	open access	-
dc.identifier.pissn	0023-6063	-
出現コレクション:	Vol.20 Part 3

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