Publication Date:
2019-08-28
Description:
A multidomain approach for calculating compressible flows by using unsteady or pseudo-unsteady methods is presented. This approach is based on a general technique of connecting together two domains in which hyperbolic systems (that may differ) are solved with the aid of compatibility relations associated with these systems. Some examples of this approach's application to calculating transonic flows in ideal fluids are shown, particularly the adjustment of shock waves. The approach is then applied to treating a shock/boundary layer interaction problem in a transonic channel.
Keywords:
AERODYNAMICS
Type:
NASA-TM-76692
,
NAS 1.15:76692
Format:
application/pdf
Permalink