In this Study, the PNS3DT code developed in the University of Glasgow to solve steady compressible parabolized Navier-Stokes equations with Baldwin-Lomax turbulence model is updated. The choice of primitive variables in the numerical scheme, different wall temperature conditions as well as the effect of different grid stretching strategies are tested in detail. Excellent agreement between the numerical and experimental results is observed. Thus, the code could provide a powerful tool to predict the aerodynamics characteristics on the ogive cylinder surface and to simulate the complicate flow structures around the cylinder
As a part of the Dutch ISNaS project our group and NLR jointly develop a flow solver for compressibl...
This paper documents an investigation of a two dimensional, incompressible Navier-Stokes solver for ...
Abstract“The PNS method is in very widespread use; indeed, it forms the basis of an industry-standar...
Renewed interest in hypersonic and supersonic flows spurred the development of the Compressible Navi...
A new computer code for the solution of the three-dimensional parabolized Navier-Stokes (PNS) equati...
This work is part of a cooperative research, development, test and evaluation program that brings sc...
A three-dimensional multiblock Navier-Stokes code, PAB3D, which was developed for propulsion integra...
Two new parabolized Navier-Stokes (PNS) codes were developed to compute the three-dimensional, visco...
A computational fluid dynamics tool has been developed capable of analyzing the viscous supersonic/h...
A grid convergence study is performed to establish benchmark solutions for turbulent flows in three ...
Two new parabolized Navier-Stokes (PNS) codes have been developed to compute the hypersonic flow of ...
The flow path of a conceptual hypersonic air-breathing scramjet engine integrated with the vehicle (...
A computer code for solving the two-dimensional compressible Navier-Stokes equations governing the s...
The parabolized stability equations (PSE) are a new and more reliable approach to analyzing the stab...
The capability of computational fluid dynamics (CFD) analysis to predict complex flowfields has been...
As a part of the Dutch ISNaS project our group and NLR jointly develop a flow solver for compressibl...
This paper documents an investigation of a two dimensional, incompressible Navier-Stokes solver for ...
Abstract“The PNS method is in very widespread use; indeed, it forms the basis of an industry-standar...
Renewed interest in hypersonic and supersonic flows spurred the development of the Compressible Navi...
A new computer code for the solution of the three-dimensional parabolized Navier-Stokes (PNS) equati...
This work is part of a cooperative research, development, test and evaluation program that brings sc...
A three-dimensional multiblock Navier-Stokes code, PAB3D, which was developed for propulsion integra...
Two new parabolized Navier-Stokes (PNS) codes were developed to compute the three-dimensional, visco...
A computational fluid dynamics tool has been developed capable of analyzing the viscous supersonic/h...
A grid convergence study is performed to establish benchmark solutions for turbulent flows in three ...
Two new parabolized Navier-Stokes (PNS) codes have been developed to compute the hypersonic flow of ...
The flow path of a conceptual hypersonic air-breathing scramjet engine integrated with the vehicle (...
A computer code for solving the two-dimensional compressible Navier-Stokes equations governing the s...
The parabolized stability equations (PSE) are a new and more reliable approach to analyzing the stab...
The capability of computational fluid dynamics (CFD) analysis to predict complex flowfields has been...
As a part of the Dutch ISNaS project our group and NLR jointly develop a flow solver for compressibl...
This paper documents an investigation of a two dimensional, incompressible Navier-Stokes solver for ...
Abstract“The PNS method is in very widespread use; indeed, it forms the basis of an industry-standar...