Applications are described of high-performance parallel, computation for the analysis of complete jet engines, considering its multi-discipline coupled problem. The coupled problem involves interaction of structures with gas dynamics, heat conduction and heat transfer in aircraft engines. The methodology issues addressed include: consistent discrete formulation of coupled problems with emphasis on coupling phenomena; effect of partitioning strategies, augmentation and temporal solution procedures; sensitivity of response to problem parameters; and methods for interfacing multiscale discretizations in different single fields. The computer implementation issues addressed include: parallel treatment of coupled systems; domain decomposition and...
Over five years of research in Computational Fluid Dynamics and its applications are covered in this...
In this paper we present several significant improvements to both coupled solution methods and sen-s...
In this paper we present several significant improvements to both coupled solution methods and sen-s...
This research program deals with the application of high-performance computing methods to the numeri...
This research program deals with the application of high-performance computing methods for the analy...
In order to predict the dynamic response of a flexible structure in a fluid flow, the equations of m...
This research program dealt with the application of high-performance computing methods to the numeri...
Applications are described of high-performance computing methods to the numerical simulation of comp...
The objective of this research is to develop computationally efficient methods for solving fluid-str...
The development of multiprocessor simulations from a serial set of ordinary differential equations d...
Phase I is complete for the development of a Computational Fluid Dynamics parallel code with automat...
Phase 1 is complete for the development of a computational fluid dynamics CFD) parallel code with au...
A procedure for computing the aeroelasticity of wings on parallel multiple-instruction, multiple-dat...
https://doi.org/10.21949/14040091996PDFResearch PaperReport NAS-96-004Computer algorithmsComputer ar...
The NASA Lewis Research Center is actively involved in the development of expert system technology t...
Over five years of research in Computational Fluid Dynamics and its applications are covered in this...
In this paper we present several significant improvements to both coupled solution methods and sen-s...
In this paper we present several significant improvements to both coupled solution methods and sen-s...
This research program deals with the application of high-performance computing methods to the numeri...
This research program deals with the application of high-performance computing methods for the analy...
In order to predict the dynamic response of a flexible structure in a fluid flow, the equations of m...
This research program dealt with the application of high-performance computing methods to the numeri...
Applications are described of high-performance computing methods to the numerical simulation of comp...
The objective of this research is to develop computationally efficient methods for solving fluid-str...
The development of multiprocessor simulations from a serial set of ordinary differential equations d...
Phase I is complete for the development of a Computational Fluid Dynamics parallel code with automat...
Phase 1 is complete for the development of a computational fluid dynamics CFD) parallel code with au...
A procedure for computing the aeroelasticity of wings on parallel multiple-instruction, multiple-dat...
https://doi.org/10.21949/14040091996PDFResearch PaperReport NAS-96-004Computer algorithmsComputer ar...
The NASA Lewis Research Center is actively involved in the development of expert system technology t...
Over five years of research in Computational Fluid Dynamics and its applications are covered in this...
In this paper we present several significant improvements to both coupled solution methods and sen-s...
In this paper we present several significant improvements to both coupled solution methods and sen-s...