Add to ORKGThis paper provides details of the Reynolds Averaged Navier-Stokes (RANS) equations based Computational Fluid Dynamics (CFD) technology developed for numerical simulation of hypersonic real gas flows. Numerical and physical aspects of such a simulation are emphasized to bring out the challenges involved. Results of validation of the RANS code on a standard configuration for which experimental data is available are discussed
The current approach to the Accurate Computation of Complex high-speed flows is to solve the Reynold...
This paper presents a review of guidelines and best practices for low-speed aerodynamic simulations ...
The objective of the present work is to develop, verify, and incorporate two equation turbulence mod...
Hypersonic vehicles are becoming more of a reality with the current level of technology. Concept veh...
The rapid and significant advances in computational power both in terms of hardware and software in ...
During reentry and hypersonic light of space vehicles through atmosphere real gas eects come into pl...
Hypersonic flows are characterised by high Mach number and high total enthalpy An elevated temperatu...
An overview is given of research activity on the application of computational fluid dynamics (CDF) f...
Several current challenges in computational fluid dynamics and aerothermodynamics for hypersonic veh...
Communication to : AIAA/ICAS international air and space symposium and exhibition, Dayton (USA), 14-...
The interest in hypersonic flow phenomena has peaked in recent years where number of experimental a...
The research objectives are to develop effective procedures for computing fluid flow at ultra high p...
AbstractDesign studies are underway for a variety of hypersonic flight vehicles. The National Aero-S...
Computational fluid dynamics computations for two hypersonic flow cases using the commercial ANSYS F...
When it comes to simulate hypersonic flows, gas-kinetic schemes provide one distinct advantage over ...
The current approach to the Accurate Computation of Complex high-speed flows is to solve the Reynold...
This paper presents a review of guidelines and best practices for low-speed aerodynamic simulations ...
The objective of the present work is to develop, verify, and incorporate two equation turbulence mod...
Hypersonic vehicles are becoming more of a reality with the current level of technology. Concept veh...
The rapid and significant advances in computational power both in terms of hardware and software in ...
During reentry and hypersonic light of space vehicles through atmosphere real gas eects come into pl...
Hypersonic flows are characterised by high Mach number and high total enthalpy An elevated temperatu...
An overview is given of research activity on the application of computational fluid dynamics (CDF) f...
Several current challenges in computational fluid dynamics and aerothermodynamics for hypersonic veh...
Communication to : AIAA/ICAS international air and space symposium and exhibition, Dayton (USA), 14-...
The interest in hypersonic flow phenomena has peaked in recent years where number of experimental a...
The research objectives are to develop effective procedures for computing fluid flow at ultra high p...
AbstractDesign studies are underway for a variety of hypersonic flight vehicles. The National Aero-S...
Computational fluid dynamics computations for two hypersonic flow cases using the commercial ANSYS F...
When it comes to simulate hypersonic flows, gas-kinetic schemes provide one distinct advantage over ...
The current approach to the Accurate Computation of Complex high-speed flows is to solve the Reynold...
This paper presents a review of guidelines and best practices for low-speed aerodynamic simulations ...
The objective of the present work is to develop, verify, and incorporate two equation turbulence mod...