9 research outputs found
On prediction of non-uniform temperature fields in heat analysis of aero engines using machine learning approach
Get PDFAuthors acknowledge support from the ESIF, EU Operational Programme Research, Develop ment and Education, and from the Center of Advanced Aerospace Technology (CZ.02.1.01/
0.0/0.0/16 019/0000826), Faculty of Mechanical Engineering, Czech Technical University in
Prague.
This work was supported by the Grant Agency of the Czech Technical University in Prague,
grant No. SGS22/151/OHK2/3T/12
Sensitivity analysis of thermodynamical parameters on the thermal bowed rotor using 2D finite element model
Get PDFCZ.02.1.01/0.0/0.0/16_019/0000826, SGS19/157/OHK2/3T/1
About the appropriate neural network size for the engineering applications
Get PDFThis work was supported by the grant agency of the Czech Technical University in Prague,
grant No. SGS22/148/OHK2/3T/12.
Authors also acknowledge support from the ESIF, EU Operational Programme Research, Devel opment and Education, and from the Center of Advanced Aerospace Technology (CZ.02.1.01/
0.0/0.0/16 019/0000826), Faculty of Mechanical Engineering, Czech Technical University in
Prague
On prediction of non-uniform temperature fields in heat analysis of aero engines using machine learning approach
No full textAuthors acknowledge support from the ESIF, EU Operational Programme Research, Develop ment and Education, and from the Center of Advanced Aerospace Technology (CZ.02.1.01/
0.0/0.0/16 019/0000826), Faculty of Mechanical Engineering, Czech Technical University in
Prague.
This work was supported by the Grant Agency of the Czech Technical University in Prague,
grant No. SGS22/151/OHK2/3T/12
Sensitivity analysis of thermodynamical parameters on the thermal bowed rotor using 2D finite element model
Get PDFCZ.02.1.01/0.0/0.0/16_019/0000826, SGS19/157/OHK2/3T/1
About the appropriate neural network size for the engineering applications
No full textThis work was supported by the grant agency of the Czech Technical University in Prague,
grant No. SGS22/148/OHK2/3T/12.
Authors also acknowledge support from the ESIF, EU Operational Programme Research, Devel opment and Education, and from the Center of Advanced Aerospace Technology (CZ.02.1.01/
0.0/0.0/16 019/0000826), Faculty of Mechanical Engineering, Czech Technical University in
Prague
