Detailed study of complex flow fields of aerodynamical configurations by using numerical methods.
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Publication:5955767
DOI10.1007/BF02812161zbMath1075.76654MaRDI QIDQ5955767
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Publication date: 18 February 2002
Published in: Sādhanā (Search for Journal in Brave)
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Cites Work
- Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods
- Approximate Riemann solvers, parameter vectors, and difference schemes
- Progress with multigrid schemes for hypersonic flow problems
- Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow
- A Numerical Method for Solving the Equations of Compressible Viscous Flow
- Generation of boundary-conforming grids around wing-body configurations using transfinite interpolation
- Upwind Second-Order Difference Schemes and Applications in Aerodynamic Flows
- An Implicit Factored Scheme for the Compressible Navier-Stokes Equations
- Numerical Computation of Vortical Flow Fields of Double‐Delta Wings Moving in a Compressible Viscous Medium
- Systems of conservation laws
- On the solution of nonlinear hyperbolic differential equations by finite differences
- Analysis of Spiraling Vortical Flows around Slender Delta Wings Moving in an Inviscid Medium
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