Assessment of meanflow solutions for instability analysis of transitioning flowsMeanflow solutions of 3D supersonic flow past a cone at incidence and a swept leading edge wing have been obtained by thre methods, viz., boundary-layer, parabolized Navier-Stokes, and thin shear-layer Navier-Stokes solvers. The smoothness and accuracy of the solution profiles are compared with a view to applying the meanflow solution to boundary-layer stability analysis.
Document ID
19910058942
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Iyer, Venkit (Vigyan, Inc. Hampton, VA, United States)