The Numerical Propulsion System Simulation (NPSS) is a full propulsion system simulation tool used by aerospace engineers to predict and analyze the aerothermodynamic behavior of commercial jet aircraft, military applications, and space transportation. The NPSS framework was developed to support aerospace, but other applications are already leveraging the initial capabilities, such as aviation safety, ground-based power, and alternative energy conversion devices such as fuel cells. By using the framework and developing the necessary components, future applications that NPSS could support include nuclear power, water treatment, biomedicine, chemical processing, and marine propulsion. NPSS will dramatically reduce the time, effort, and expens...
As part of the National Cycle Program (NCP), a powerful new numerical solver has been developed to s...
Within NASA's High Performance Computing and Communication (HPCC) program, NASA Glenn Research Cente...
A major difficulty in designing aeropropulsion systems is that of identifying and understanding the ...
The NASA Glenn Research Center is developing an advanced multidisciplinary analysis environment for ...
Advances in computational technology and in physics-based modeling are making large scale, detailed ...
Producing a new aircraft engine currently costs approximately $1 billion, with 3 years of developmen...
The NASA Lewis Research Center is developing an environment for analyzing and designing aircraft eng...
The technologies necessary to enable detailed numerical simulations of complete propulsion systems a...
Advances in computational technology and in physics-based modeling are making large-scale, detailed ...
The tremendous progress being made in computational engineering and the rapid growth in computing po...
This talk presents Pratt and Whitney's space division overview of the Numerical Propulsion System Si...
The technologies necessary to enable detailed numerical simulations of complete propulsion systems a...
NASA-Lewis has committed to a long range goal of creating a numerical test cell for aeropropulsion r...
An altitude test facility was modeled using Numerical Propulsion System Simulation (NPSS). This alti...
During the preliminary or conceptual design phase of an aircraft engine, the turbomachinery designer...
As part of the National Cycle Program (NCP), a powerful new numerical solver has been developed to s...
Within NASA's High Performance Computing and Communication (HPCC) program, NASA Glenn Research Cente...
A major difficulty in designing aeropropulsion systems is that of identifying and understanding the ...
The NASA Glenn Research Center is developing an advanced multidisciplinary analysis environment for ...
Advances in computational technology and in physics-based modeling are making large scale, detailed ...
Producing a new aircraft engine currently costs approximately $1 billion, with 3 years of developmen...
The NASA Lewis Research Center is developing an environment for analyzing and designing aircraft eng...
The technologies necessary to enable detailed numerical simulations of complete propulsion systems a...
Advances in computational technology and in physics-based modeling are making large-scale, detailed ...
The tremendous progress being made in computational engineering and the rapid growth in computing po...
This talk presents Pratt and Whitney's space division overview of the Numerical Propulsion System Si...
The technologies necessary to enable detailed numerical simulations of complete propulsion systems a...
NASA-Lewis has committed to a long range goal of creating a numerical test cell for aeropropulsion r...
An altitude test facility was modeled using Numerical Propulsion System Simulation (NPSS). This alti...
During the preliminary or conceptual design phase of an aircraft engine, the turbomachinery designer...
As part of the National Cycle Program (NCP), a powerful new numerical solver has been developed to s...
Within NASA's High Performance Computing and Communication (HPCC) program, NASA Glenn Research Cente...
A major difficulty in designing aeropropulsion systems is that of identifying and understanding the ...