Leading edge bluntness effect on the flow in a model air-inlet
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Publication:477224
DOI10.1134/S0015462814040061zbMath1301.76003MaRDI QIDQ477224
I. V. Struminskaya, V. Ya. Borovoj, V. E. Mosharov, A. S. Skuratov, V. N. Radchenko
Publication date: 2 December 2014
Published in: Fluid Dynamics (Search for Journal in Brave)
experimentshockheat transferboundary layerhypersonic flowinterferenceboundary layer separationentropy layerpanoramic measurements
Experimental work for problems pertaining to fluid mechanics (76-05) Shock waves and blast waves in fluid mechanics (76L05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)
Related Items (2)
Hysteresis of shock wave locations in divergent bent channels ⋮ Numerical study of bluntness effects on laminar leading edge separation in hypersonic flow
Cites Work
- Interaction of intersecting shocks with a flat-plate boundary layer in the presence of an entropy layer
- Interaction between an inclined shock and boundary and high-entropy layers on a flat plate
- Two-dimensional interaction between an incident shock and a turbulent boundary layer in the presence of an entropy layer
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