ABSTRACT This best practice guide provides information about Intel's MIC architecture and... more ABSTRACT This best practice guide provides information about Intel's MIC architecture and programming models for the Intel Xeon Phi coprocessor in order to enable programmers to achieve good performance of their pplications. The guide covers a wide range of topics from the description of the hardware of the Intel Xeon Phi coprocessor through information about the basic programming models as well as information about porting programs up to tools and strategies how to analyze and improve the performance of applications.
2018 International Conference on High Performance Computing & Simulation (HPCS), 2018
Automatic multidisciplinary design optimization is one of the challenges that are faced in the pr... more Automatic multidisciplinary design optimization is one of the challenges that are faced in the processes involved in designing efficient wings for aircraft. In this paper we present mixed fidelity aerodynamic and aero-structural optimization methods for designing wings. A novel shape design methodology has been developed - it is based on a mix of the automatic aerodynamic optimization for a reference aircraft model, and the aero-structural optimization for an uninhabited air vehicle (UAV) with a high aspect ratio wing. This paper is a significant step towards making it possible to perform all the core processes for aerodynamic and aero-structural optimization that require special skills in a fully automatic manner - this covers all the processes from creating the mesh for the wing simulation to executing the high-fidelity computational fluid dynamics (CFD) analysis code. Our results confirm that the simulation tools can make it possible for a far broader range of engineering researc...
Airinnova is a start-up company with a key competency in the automation of high fidelity computat... more Airinnova is a start-up company with a key competency in the automation of high fidelity computational fluid<br> dynamics (CFD) analysis. The goal of this SHAPE project, a collaboration with the PDC Center for High<br> Performance Computing at the KTH Royal Institute of Technology (KTH-PDC), was to develop automated<br> procedures for carrying out CFD analysis in the field of aerodynamic optimization and design. The project is a<br> significant step towards automation of the core processes that ordinarily would require specialist skills, such as<br> creation of the simulation mesh, thus assisting a broader sphere of engineers to design aircraft in more efficient<br> and simpler ways.
This document describes the work undertaken by Task 7.2 "Joint Access to Data, HTC and Cloud... more This document describes the work undertaken by Task 7.2 "Joint Access to Data, HTC and Cloud Computing Resources" within the EUDAT2020 project focusing on the interoperability between EUDAT and EGI. The main objective of the conducted work was to realize cross-infrastructure services that enable the desired perceived seamless access to a combined infrastructure offering by both EGI and EUDAT services in pairing their data and high-throughput computing resources together. This document concentrates on the phase after the definition of the generic use case and depicts in detail the challenges encountered by the early adopters, the resulting new requirements and the identified solutions.
2018 International Conference on High Performance Computing & Simulation (HPCS)
Automatic multidisciplinary design optimization is one of the challenges that are faced in the pr... more Automatic multidisciplinary design optimization is one of the challenges that are faced in the processes involved in designing efficient wings for aircraft. In this paper we present mixed fidelity aerodynamic and aero-structural optimization methods for designing wings. A novel shape design methodology has been developed - it is based on a mix of the automatic aerodynamic optimization for a reference aircraft model, and the aero-structural optimization for an uninhabited air vehicle (UAV) with a high aspect ratio wing. This paper is a significant step towards making it possible to perform all the core processes for aerodynamic and aero-structural optimization that require special skills in a fully automatic manner - this covers all the processes from creating the mesh for the wing simulation to executing the high-fidelity computational fluid dynamics (CFD) analysis code. Our results confirm that the simulation tools can make it possible for a far broader range of engineering researchers and developers to design aircraft in much simpler and more efficient ways. This is a vital step in the evolution of wing design processes as it means that the extremely expensive laboratory experiments that were traditionally used when designing the wings can now be replaced with more cost effective high performance computing (HPC) simulation that utilize accurate numerical methods.
2020 28th Euromicro International Conference on Parallel, Distributed and Network-Based Processing (PDP), 2020
In this paper, an automation process to perform Reynolds-Averaged Navier-Stokes (RANS) computatio... more In this paper, an automation process to perform Reynolds-Averaged Navier-Stokes (RANS) computational fluid dynamics (CFD) analysis is developed to carry out aerodynamic design and optimization. The aircraft model/geometry is defined by a Common Parametric Aircraft Configuration Schema (CPACS) file, and the analyses are facilitated using high performance computers (HPC). As the computational capability of the available HPC systems is a limiting factor in the complexity of analyses that can be performed, a detailed performance analysis of the open source CFD code SU2 is undertaken and the profiling and performance analyses for large simulations are carried out.
This Best Practice Guide provides information about Intel’s MIC architecture and programming mode... more This Best Practice Guide provides information about Intel’s MIC architecture and programming models for the first generation Intel® Xeon Phi™ coprocessor named Knights Corner (KNC) in order to enable programmers to achieve good performance out of their applications. The guide covers a wide range of topics from the description of the hardware of the Intel® Xeon Phi™ coprocessor through information about the basic programming models as well as information about porting programs up to tools and strategies how to analyse and improve the performance of applications. The guide was created based on the PRACE-3IP Intel® Xeon Phi™ Best Practice Guide. New is the inclusion of information about European Intel® Xeon Phi™ based systems. The following systems are now described: •Avitohol @ IICT-BAS, Bulgary, MareNostrum @ BSC, Spain, Salomon @ IT4Innovations, Czech Republic, SuperMIC @ LRZ, Germany. Furthermore, the following new sections are included: OpenMP 4.x Offloading, OpenCL, Intel Cilk Plus / MYO, Information about some selected applications ported to Intel® Xeon Phi™, Benchmark results using e.g. the PRACE Accelerator Benchmark Suite. Several existing sections have been updated to reflect recent changes.
Airinnova is a start-up company with a key competency in the automation of high-fidelity computat... more Airinnova is a start-up company with a key competency in the automation of high-fidelity computational fluid dynamics (CFD) analysis. Following on from our previous PRACE SHAPE project, we have continued collaborating with the PDC Center for High Performance Computing at the KTH Royal Institute of Technology (KTH-PDC), to investigate the performance analysis of the open source CFD code SU2 and further develop the automation process for the field of aerodynamic optimization and design.
While in the past spheroidicity was assumed, and still is used in modeling of most nebulae, we kn... more While in the past spheroidicity was assumed, and still is used in modeling of most nebulae, we know now that only a small number of planetary nebulae (PNe) are really spherical or at least nearly round. Round planetary nebulae are the minority of objects. In case of those objects that underwent a very late helium flash (called VLTP or &quot;born-again&quot; PNe) it seems to be different. The first, hydrogen rich PN, is more or less round. The ejecta from the VLTP event is extremely asymmetrically. Angular momentum is mostly assumed to be the main reason for the asymmetry in PNe. Thus we have to find processes either changing their behavior within a few hundred to a few thousands of years or change their properties dramatically due to the variation of the abundance. They most likely have a strong link or dependency with the abundance of the ejecta.
While in the past spheroidicity was assumed, and still is used in modeling of most nebulae, we kn... more While in the past spheroidicity was assumed, and still is used in modeling of most nebulae, we know now that only a small number of planetary nebulae (PNe) are really spherical or at least nearly round. Round planetary nebulae are the minority of objects. In case of those objects that underwent a very late helium flash (called VLTP or "born-again" PNe) it seems to be different. The first, hydrogen rich PN, is more or less round. The ejecta from the VLTP event is extremely asymmetrically. Angular momentum is mostly assumed to be the main reason for the asymmetry in PNe. Thus we have to find processes either changing their behavior within a few hundred to a few thousands of years or change their properties dramatically due to the variation of the abundance. They most likely have a strong link or dependency with the abundance of the ejecta.
This best practice guide provides information about Intel's MIC architecture and programming ... more This best practice guide provides information about Intel's MIC architecture and programming models for the Intel Xeon Phi coprocessor in order to enable programmers to achieve good performance of their pplications. The guide covers a wide range of topics from the description of the hardware of the Intel Xeon Phi coprocessor through information about the basic programming models as well as information about porting programs up to tools and strategies how to analyze and improve the performance of applications.
Airinnova is a start-up company with a key competency in the automation of high fidelity computat... more Airinnova is a start-up company with a key competency in the automation of high fidelity computational fluid dynamics (CFD) analysis. The goal of this SHAPE project, a collaboration with the PDC Center for High Performance Computing at the KTH Royal Institute of Technology (KTH-PDC), was to develop automated procedures for carrying out CFD analysis in the field of aerodynamic optimization and design. The project is a significant step towards automation of the core processes that ordinarily would require specialist skills, such as creation of the simulation mesh, thus assisting a broader sphere of engineers to design aircraft in more efficient and simpler ways.
This Best Practice Guide provides information about Intel’s MIC architecture and programming mode... more This Best Practice Guide provides information about Intel’s MIC architecture and programming models for the first generation Intel® Xeon Phi™ coprocessor named Knights Corner (KNC) in order to enable programmers to achieve good performance out of their applications. The guide covers a wide range of topics from the description of the hardware of the Intel® Xeon Phi™ coprocessor through information about the basic programming models as well as information about porting programs up to tools and strategies how to analyse and improve the performance of applications. The guide was created based on the PRACE-3IP Intel® Xeon Phi™ Best Practice Guide. New is the inclusion of information about European Intel® Xeon Phi™ based systems. The following systems are now described: •Avitohol @ IICT-BAS, Bulgary, MareNostrum @ BSC, Spain, Salomon @ IT4Innovations, Czech Republic, SuperMIC @ LRZ, Germany. Furthermore, the following new sections are included: OpenMP 4.x Offloading, OpenCL, Intel Cilk Plus / MYO, Information about some selected applications ported to Intel® Xeon Phi™, Benchmark results using e.g. the PRACE Accelerator Benchmark Suite. Several existing sections have been updated to reflect recent changes.
This best practice guide provides information about Intel's MIC architecture and programming ... more This best practice guide provides information about Intel's MIC architecture and programming models for the Intel Xeon Phi coprocessor in order to enable programmers to achieve good performance of their pplications. The guide covers a wide range of topics from the description of the hardware of the Intel Xeon Phi coprocessor through information about the basic programming models as well as information about porting programs up to tools and strategies how to analyze and improve the performance of applications.
ABSTRACT This best practice guide provides information about Intel&#39;s MIC architecture and... more ABSTRACT This best practice guide provides information about Intel&#39;s MIC architecture and programming models for the Intel Xeon Phi coprocessor in order to enable programmers to achieve good performance of their pplications. The guide covers a wide range of topics from the description of the hardware of the Intel Xeon Phi coprocessor through information about the basic programming models as well as information about porting programs up to tools and strategies how to analyze and improve the performance of applications.
2018 International Conference on High Performance Computing & Simulation (HPCS), 2018
Automatic multidisciplinary design optimization is one of the challenges that are faced in the pr... more Automatic multidisciplinary design optimization is one of the challenges that are faced in the processes involved in designing efficient wings for aircraft. In this paper we present mixed fidelity aerodynamic and aero-structural optimization methods for designing wings. A novel shape design methodology has been developed - it is based on a mix of the automatic aerodynamic optimization for a reference aircraft model, and the aero-structural optimization for an uninhabited air vehicle (UAV) with a high aspect ratio wing. This paper is a significant step towards making it possible to perform all the core processes for aerodynamic and aero-structural optimization that require special skills in a fully automatic manner - this covers all the processes from creating the mesh for the wing simulation to executing the high-fidelity computational fluid dynamics (CFD) analysis code. Our results confirm that the simulation tools can make it possible for a far broader range of engineering researc...
Airinnova is a start-up company with a key competency in the automation of high fidelity computat... more Airinnova is a start-up company with a key competency in the automation of high fidelity computational fluid<br> dynamics (CFD) analysis. The goal of this SHAPE project, a collaboration with the PDC Center for High<br> Performance Computing at the KTH Royal Institute of Technology (KTH-PDC), was to develop automated<br> procedures for carrying out CFD analysis in the field of aerodynamic optimization and design. The project is a<br> significant step towards automation of the core processes that ordinarily would require specialist skills, such as<br> creation of the simulation mesh, thus assisting a broader sphere of engineers to design aircraft in more efficient<br> and simpler ways.
This document describes the work undertaken by Task 7.2 "Joint Access to Data, HTC and Cloud... more This document describes the work undertaken by Task 7.2 "Joint Access to Data, HTC and Cloud Computing Resources" within the EUDAT2020 project focusing on the interoperability between EUDAT and EGI. The main objective of the conducted work was to realize cross-infrastructure services that enable the desired perceived seamless access to a combined infrastructure offering by both EGI and EUDAT services in pairing their data and high-throughput computing resources together. This document concentrates on the phase after the definition of the generic use case and depicts in detail the challenges encountered by the early adopters, the resulting new requirements and the identified solutions.
2018 International Conference on High Performance Computing & Simulation (HPCS)
Automatic multidisciplinary design optimization is one of the challenges that are faced in the pr... more Automatic multidisciplinary design optimization is one of the challenges that are faced in the processes involved in designing efficient wings for aircraft. In this paper we present mixed fidelity aerodynamic and aero-structural optimization methods for designing wings. A novel shape design methodology has been developed - it is based on a mix of the automatic aerodynamic optimization for a reference aircraft model, and the aero-structural optimization for an uninhabited air vehicle (UAV) with a high aspect ratio wing. This paper is a significant step towards making it possible to perform all the core processes for aerodynamic and aero-structural optimization that require special skills in a fully automatic manner - this covers all the processes from creating the mesh for the wing simulation to executing the high-fidelity computational fluid dynamics (CFD) analysis code. Our results confirm that the simulation tools can make it possible for a far broader range of engineering researchers and developers to design aircraft in much simpler and more efficient ways. This is a vital step in the evolution of wing design processes as it means that the extremely expensive laboratory experiments that were traditionally used when designing the wings can now be replaced with more cost effective high performance computing (HPC) simulation that utilize accurate numerical methods.
2020 28th Euromicro International Conference on Parallel, Distributed and Network-Based Processing (PDP), 2020
In this paper, an automation process to perform Reynolds-Averaged Navier-Stokes (RANS) computatio... more In this paper, an automation process to perform Reynolds-Averaged Navier-Stokes (RANS) computational fluid dynamics (CFD) analysis is developed to carry out aerodynamic design and optimization. The aircraft model/geometry is defined by a Common Parametric Aircraft Configuration Schema (CPACS) file, and the analyses are facilitated using high performance computers (HPC). As the computational capability of the available HPC systems is a limiting factor in the complexity of analyses that can be performed, a detailed performance analysis of the open source CFD code SU2 is undertaken and the profiling and performance analyses for large simulations are carried out.
This Best Practice Guide provides information about Intel’s MIC architecture and programming mode... more This Best Practice Guide provides information about Intel’s MIC architecture and programming models for the first generation Intel® Xeon Phi™ coprocessor named Knights Corner (KNC) in order to enable programmers to achieve good performance out of their applications. The guide covers a wide range of topics from the description of the hardware of the Intel® Xeon Phi™ coprocessor through information about the basic programming models as well as information about porting programs up to tools and strategies how to analyse and improve the performance of applications. The guide was created based on the PRACE-3IP Intel® Xeon Phi™ Best Practice Guide. New is the inclusion of information about European Intel® Xeon Phi™ based systems. The following systems are now described: •Avitohol @ IICT-BAS, Bulgary, MareNostrum @ BSC, Spain, Salomon @ IT4Innovations, Czech Republic, SuperMIC @ LRZ, Germany. Furthermore, the following new sections are included: OpenMP 4.x Offloading, OpenCL, Intel Cilk Plus / MYO, Information about some selected applications ported to Intel® Xeon Phi™, Benchmark results using e.g. the PRACE Accelerator Benchmark Suite. Several existing sections have been updated to reflect recent changes.
Airinnova is a start-up company with a key competency in the automation of high-fidelity computat... more Airinnova is a start-up company with a key competency in the automation of high-fidelity computational fluid dynamics (CFD) analysis. Following on from our previous PRACE SHAPE project, we have continued collaborating with the PDC Center for High Performance Computing at the KTH Royal Institute of Technology (KTH-PDC), to investigate the performance analysis of the open source CFD code SU2 and further develop the automation process for the field of aerodynamic optimization and design.
While in the past spheroidicity was assumed, and still is used in modeling of most nebulae, we kn... more While in the past spheroidicity was assumed, and still is used in modeling of most nebulae, we know now that only a small number of planetary nebulae (PNe) are really spherical or at least nearly round. Round planetary nebulae are the minority of objects. In case of those objects that underwent a very late helium flash (called VLTP or &quot;born-again&quot; PNe) it seems to be different. The first, hydrogen rich PN, is more or less round. The ejecta from the VLTP event is extremely asymmetrically. Angular momentum is mostly assumed to be the main reason for the asymmetry in PNe. Thus we have to find processes either changing their behavior within a few hundred to a few thousands of years or change their properties dramatically due to the variation of the abundance. They most likely have a strong link or dependency with the abundance of the ejecta.
While in the past spheroidicity was assumed, and still is used in modeling of most nebulae, we kn... more While in the past spheroidicity was assumed, and still is used in modeling of most nebulae, we know now that only a small number of planetary nebulae (PNe) are really spherical or at least nearly round. Round planetary nebulae are the minority of objects. In case of those objects that underwent a very late helium flash (called VLTP or "born-again" PNe) it seems to be different. The first, hydrogen rich PN, is more or less round. The ejecta from the VLTP event is extremely asymmetrically. Angular momentum is mostly assumed to be the main reason for the asymmetry in PNe. Thus we have to find processes either changing their behavior within a few hundred to a few thousands of years or change their properties dramatically due to the variation of the abundance. They most likely have a strong link or dependency with the abundance of the ejecta.
This best practice guide provides information about Intel's MIC architecture and programming ... more This best practice guide provides information about Intel's MIC architecture and programming models for the Intel Xeon Phi coprocessor in order to enable programmers to achieve good performance of their pplications. The guide covers a wide range of topics from the description of the hardware of the Intel Xeon Phi coprocessor through information about the basic programming models as well as information about porting programs up to tools and strategies how to analyze and improve the performance of applications.
Airinnova is a start-up company with a key competency in the automation of high fidelity computat... more Airinnova is a start-up company with a key competency in the automation of high fidelity computational fluid dynamics (CFD) analysis. The goal of this SHAPE project, a collaboration with the PDC Center for High Performance Computing at the KTH Royal Institute of Technology (KTH-PDC), was to develop automated procedures for carrying out CFD analysis in the field of aerodynamic optimization and design. The project is a significant step towards automation of the core processes that ordinarily would require specialist skills, such as creation of the simulation mesh, thus assisting a broader sphere of engineers to design aircraft in more efficient and simpler ways.
This Best Practice Guide provides information about Intel’s MIC architecture and programming mode... more This Best Practice Guide provides information about Intel’s MIC architecture and programming models for the first generation Intel® Xeon Phi™ coprocessor named Knights Corner (KNC) in order to enable programmers to achieve good performance out of their applications. The guide covers a wide range of topics from the description of the hardware of the Intel® Xeon Phi™ coprocessor through information about the basic programming models as well as information about porting programs up to tools and strategies how to analyse and improve the performance of applications. The guide was created based on the PRACE-3IP Intel® Xeon Phi™ Best Practice Guide. New is the inclusion of information about European Intel® Xeon Phi™ based systems. The following systems are now described: •Avitohol @ IICT-BAS, Bulgary, MareNostrum @ BSC, Spain, Salomon @ IT4Innovations, Czech Republic, SuperMIC @ LRZ, Germany. Furthermore, the following new sections are included: OpenMP 4.x Offloading, OpenCL, Intel Cilk Plus / MYO, Information about some selected applications ported to Intel® Xeon Phi™, Benchmark results using e.g. the PRACE Accelerator Benchmark Suite. Several existing sections have been updated to reflect recent changes.
This best practice guide provides information about Intel's MIC architecture and programming ... more This best practice guide provides information about Intel's MIC architecture and programming models for the Intel Xeon Phi coprocessor in order to enable programmers to achieve good performance of their pplications. The guide covers a wide range of topics from the description of the hardware of the Intel Xeon Phi coprocessor through information about the basic programming models as well as information about porting programs up to tools and strategies how to analyze and improve the performance of applications.
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