Propagation of perturbations in the three-dimensional boundary layer on a delta wing in the viscid-inviscid interaction regime

DOI10.1134/S0015462810030099zbMath1215.76071MaRDI QIDQ545805

K. T. M'int, G. N. Dudin

Publication date: 22 June 2011

Published in: Fluid Dynamics (Search for Journal in Brave)

zbMATH Keywords

boundary layerdelta winghypersonic streampropagation of perturbationsstrong interaction

Mathematics Subject Classification ID

Viscous-inviscid interaction for compressible fluids and gas dynamics (76N17) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

• Formation of supercritical flow regions on low-aspect-ratio wings
• A method of calculating a regime of strong viscous interaction on a delta wing
• Calculation of three-dimensional boundary layer on a triangular plate of finite length in a hypersonic stream
• Aspects of ’’multitime initial-value problem’’ originating from boundary layer equations
• On the determination of the zones of influence and dependence for three-dimensional boundary-layer equations
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