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  • The article deals with design and numerical calculation of a variable test section for small supersonic wind tunnel. The supersonic wind tunnel is designed to be driven by a supersonic ejector. The test section, which is in focus, is considered to by placed on its suction inlet. Schlieren method will be used to investigate the flow within. The purpose of the test section is to demonstrate effects, which occur in supersonic flows, e.g. shock waves, interactions of shock waves with boundary layers etc.
  • The article deals with design and numerical calculation of a variable test section for small supersonic wind tunnel. The supersonic wind tunnel is designed to be driven by a supersonic ejector. The test section, which is in focus, is considered to by placed on its suction inlet. Schlieren method will be used to investigate the flow within. The purpose of the test section is to demonstrate effects, which occur in supersonic flows, e.g. shock waves, interactions of shock waves with boundary layers etc. (en)
Title
  • Design and Numerical Calculation of Variable Test Section for Small Supersonic Wind Tunnel
  • Design and Numerical Calculation of Variable Test Section for Small Supersonic Wind Tunnel (en)
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  • Design and Numerical Calculation of Variable Test Section for Small Supersonic Wind Tunnel
  • Design and Numerical Calculation of Variable Test Section for Small Supersonic Wind Tunnel (en)
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  • RIV/46747885:24210/10:#0001635!RIV11-MSM-24210___
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  • I, Z(MSM4674788501)
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  • 253491
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  • RIV/46747885:24210/10:#0001635
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  • shock waves; supersonic ejector; Schlieren method (en)
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  • [ACE2D7139542]
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  • Rožnov pod Radhoštěm
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  • Vysoká škola báňská - TU Ostrava
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  • XXIX. setkání kateder mechaniky tekutin a termomechaniky
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  • Dvořák, Václav
  • Kolář, Jan
  • Stupka, Oldřich
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  • Vysoká škola báňská - Technická univerzita Ostrava
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  • 9788024822440
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  • 24210
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