NEARZEUS CFD: Code for detailed missile aerodynamics, valid for supersonic/hypersonic flow. Predicts nonlinear details of flow surrounding the missile. Finite-volume Godunov scheme, second order accurate. Zonal Euler Solver, supersonic space marching, real gas option. External or internal flows, multiple zone semi-automatic gridding.
ZEUSBL: Boundary layer module for NEARZEUS, aerodynamic heating.
These codes run fast on workstations and provide accurate dynamic characteristics and skin friction/heat transfer estimates for high Mach number configurations. Reduces the requirements for high speed wind tunnel tests in designing new concepts.
Stanley Perkins
Senior Research Engineer
Nielsen Engineering & Research, Inc.
526 Clyde Avenue
Mountain View, CA 94043-2212
USA
415-968-9457
415-968-1410 (fax)
scp@nearinc.com
For applications in related solution areas, see the following indices: Aerodynamics, Aerospace, Analysis, Engineering, the developer index for Nielsen Engineering & Research, Inc. and the market segment index for Computational Fluid Dynamics (CFD).
