Multiphysics Simulation for Hypersonic Vehicle Design
Ansys simulation tools are perfect solutions to examine all the challenges of hypersonic speed. As an aircraft begins to travel above Mach 1, fluids start to exhibit different physical behavior. Our multiphysics simulations enable users to capture the complex phenomena that occur, including strong shocks, plasma, ablation, structural deformation and chemical nonequilibrium. Shorten your development time and reduce testing efforts with industry-leading software that allows you to quickly tackle problems specific to hypersonic design.
CFD software known for its advanced physics modeling and renowned for industry leading accuracy.
Solve broad structural analysis needs with a suite of finite element analysis (FEA) solutions that provides in-depth analysis of structural and coupled-field behaviors.
A 3D electromagnetic field solver to design high-frequency and high-speed electronic components. Its FEM, IE, asymptotic and hybrid solvers address RF, microwave, IC, PCB and EMI problems.
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At hypersonic speeds, many challenges may arise that need to be closely examined. There are so few wind tunnels in the world capable of testing hypersonic prototypes, and flight testing is extremely expensive and lengthy. Simulation offers the best and most cost-effective way to look at this flight regime. Ansys simulation tools can be used to examine all the challenges associated with hypersonic speed.
Ansys simulation tools can be used to examine all the challenges one may face while traveling at hypersonic speed.
This webinar will consider a typical sounding rocket with simplified internal components subjected to atmospheric re-entry aerodynamic conditions. It will illustrate the capabilities and workflow approaches that can be used to evaluate the thermal performance using Ansys structural and CFD simulation tools connected via the Ansys Systems Coupling environment.
In this on-demand webinar, we focus on the numerical study of the external aerodynamics of two cruise missile geometries. The first is a generic high-supersonic/low-hypersonic geometry. The study analyzes the main flow features to better understand the physical phenomena that govern the behavior of canard geometries at different angles of attack.
