نتائج البحث - David Simurda

REGARDING CERTAIN AERODYNAMIC SOURCES OF NON-STATIONARY FORCE LOADS ON TURBINE PROFILES حسب Tomáš Radnic, Martin Luxa, David Šimurda

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Pressure Losses Downstream of a Compact Valve in the Inlet Chamber of an Intermediate-Pressure Steam Turbine حسب Vaclav Slama, David Simurda, Richard Lenhard

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Shock wave configuration in a transonic flow through a mid-section of a last stage turbine blade cascade equipped with a part-span connector حسب Tomáš Radnic, Pavel Šafařík, Martin Luxa, David Šimurda

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Causes and Solution of Aperiodicity of Supersonic Flow Field Downstream of a Profile Cascade حسب Martin Luxa, Jaroslav Synac, Pavel Safarik, David Simurda

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Experimental Visualization of Unsteady Flow in a Transonic Oscillating-Blade Compressor Cascade Using High-Speed Two-Wavelength Interferometry حسب Jindřich Hála, Pavel Psota, David Šimurda, Jan Lepicovsky

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AERODYNAMIC RESEARCH ON THE MIDSECTION OF A LONG TURBINE BLADE حسب DAVID SIMURDA, MARTIN LUXA, PAVEL SAFARˇ´IK, JAROSLAV SYNA´C

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Aerodynamic response of a blade cascade to torsional excitation of one blade at subsonic and transonic velocities حسب David Šimurda, Jiří Fürst, Josef Musil, Petr Šidlof, Jan Lepicovsky

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Computational study of flow separation in truncated ideal contour nozzles under high-altitude conditions حسب Ijas Muhammed, V V, Shamsia Banu N, Abhilash Suryan, Vincent Lijo, David Simurda, Heuy Dong Kim

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Characterization of Supersonic Compressible Fluid Flow Using High-Speed Interferometry حسب Pavel Psota, Gramoz Çubreli, Jindřich Hála, David Šimurda, Petr Šidlof, Jan Kredba, Marek Stašík, Vít Lédl, Michal Jiránek, Martin Luxa, Jan Lepicovsky

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