Search results
- 1.0458760 - ÚT 2017 RIV US eng J - Journal Article
Luxa, Martin - Příhoda, Jaromír - Šimurda, David - Straka, P. - Synáč, J.
Investigation of the Compressible Flow through the Tip-Section Turbine Blade Cascade with Supersonic Inlet.
Journal of Thermal Science. Roč. 25, č. 2 (2016), s. 138-144. ISSN 1003-2169. E-ISSN 1993-033X
R&D Projects: GA TA ČR(CZ) TA03020277; GA ČR GAP101/12/1271
Institutional support: RVO:61388998
Keywords : long turbine rotor blade * supersonic tip section * optical methods * transition modelling * CFD
Subject RIV: BK - Fluid Dynamics
Impact factor: 0.678, year: 2016
Permanent Link: http://hdl.handle.net/11104/0259005 - 2.0453406 - ÚT 2016 RIV CZ eng V - Research Report
Luxa, Martin - Šimurda, David
Measurement on TR-U-6 Cascade - Appendix.
Praha: Doosan Škoda Power s.r.o, 2015. 32 s. Z-1540/15.
Source of funding: N - Non-public resources
Keywords : tip section * long turbine rotor blade * transonic flow
Subject RIV: BK - Fluid Dynamics
Permanent Link: http://hdl.handle.net/11104/0255302 - 3.0446260 - ÚT 2016 IT eng C - Conference Paper (international conference)
Váchová, J. - Luxa, Martin - Příhoda, Jaromír - Šimurda, David
Transition Model Application on Mid-Section Turbine Blade Cascade.
Proceedings of the 12th International Symposium on Experimental Computational Aerothermodynamics of Internal Flows. Lerici, 2015, s. 1-8.
[International Symposium on Experimental Computational Aerothermodynamics of Internal Flows : ISAIF /12./. Lerici (IT), 13.07.2015-16.07.2015]
R&D Projects: GA TA ČR(CZ) TA03020277; GA ČR GAP101/12/1271
Institutional support: RVO:61388998
Keywords : blade cascade * long turbine rotor blade * mid-section * optical methods * CFD modelling
Subject RIV: BK - Fluid Dynamics
Permanent Link: http://hdl.handle.net/11104/0254455 - 4.0446259 - ÚT 2016 IT eng C - Conference Paper (international conference)
Luxa, Martin - Příhoda, Jaromír - Šimurda, David - Straka, P. - Synáč, J.
Investigation of the Compressible Flow through the Tip-Section Turbine Blade Cascade with Supersonic Inlet.
Proceedings of the 12th International Symposium on Experimental Computational Aerothermodynamics of Internal Flows. Lerici, 2015, s. 1-8.
[International Symposium on Experimental Computational Aerothermodynamics of Internal Flows : ISAIF /12./. Lerici (IT), 13.07.2015-16.07.2015]
R&D Projects: GA TA ČR(CZ) TA03020277; GA ČR GAP101/12/1271
Institutional support: RVO:61388998
Keywords : long turbine rotor blade * supersonic tip section * optical methods * transition modelling * CFD
Subject RIV: BK - Fluid Dynamics
Permanent Link: http://hdl.handle.net/11104/0254458 - 5.0432289 - ÚT 2015 RIV CZ eng K - Conference Paper (Czech conference)
Luxa, Martin - Synáč, J. - Šimurda, David - Šafařík, Pavel
Aerodynamic Data for Tip Section of Rotor with 52 Titanium Blades 1375 mm Long.
Turbostroje 2014 - Sborník referátů. Plzeň: ZČU Plzeň, 2014. ISBN 978-80-260-6447-3.
[Turbostroje 2014. Plzeň (CZ), 24.09.2014-25.09.2014]
R&D Projects: GA TA ČR(CZ) TA03020277
Institutional support: RVO:61388998
Keywords : supersonic flow * long turbine rotor blade * tip section
Subject RIV: BK - Fluid Dynamics
Permanent Link: http://hdl.handle.net/11104/0240309