Pages that link to "Item:Q266099"
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The following pages link to Complex conservative difference schemes for computing supersonic flows past simple aerodynamic forms (Q266099):
Displaying 6 items.
- Compact finite difference schemes for the Euler and Navier-Stokes equations (Q1054542) (← links)
- Computation of steady supersonic flows by a flux-difference/splitting method (Q1069378) (← links)
- Propagation of a shock wave through a viscous heat-conducting gas in a long microchannel (Q2322140) (← links)
- Conservative upwind difference schemes for compressible flows in a duct (Q2519525) (← links)
- The use of high-order composite compact schemes for computing supersonic jet interaction with a surface (Q5413228) (← links)
- Toward the ultimate conservative scheme: Following the quest (Q5937907) (← links)