Aerodynamic Force Measurement Technique of Free-Flying Model in a Shock Tunnel

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dc.contributor.authorCHOI, ILSUNGko
dc.contributor.authorPARK, GISUko
dc.date.accessioned2022-09-07T08:00:32Z-
dc.date.available2022-09-07T08:00:32Z-
dc.date.created2022-08-04-
dc.date.issued2022-07-07-
dc.identifier.citation32nd International Symposium on Rarefied Gas Dynamics-
dc.identifier.urihttp://hdl.handle.net/10203/298439-
dc.languageEnglish-
dc.publisherKorean Society of Computatuonal Fluids Engineering-
dc.titleAerodynamic Force Measurement Technique of Free-Flying Model in a Shock Tunnel-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationname32nd International Symposium on Rarefied Gas Dynamics-
dc.identifier.conferencecountryKO-
dc.identifier.conferencelocationHotel Le Meridien, Seoul-
dc.contributor.localauthorPARK, GISU-
dc.contributor.nonIdAuthorCHOI, ILSUNG-
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AE-Conference Papers(학술회의논문)
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