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Observation of transonic shock tube airfoil flow with focusing schlieren method
D111 フォーカシングシュリーレン法による遷音速衝撃波管翼型回りの観察
2004
Transactions of Visualization Society of Japan
D111 フォーカシングシュリーレン法による遷音速衝撃波管翼型回りの観察
Preserved Fulltext
In this study, the focusing schleren system was designed to visualize the flow field around the double wedge airfoil model in the test section of the shock tube. The focusing schlieren system was
doi:10.3154/jvs.24.supplement1_157
fatcat:ck67gkawtrcrlghne2etxtifpi