Pages that link to "Item:Q3122274"
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The following pages link to Numerical Investigations of Effusion Cooling in Hypersonic Boundary-Layer Flow (Q3122274):
Displaying 5 items.
- LES investigation of the flow through an effusion-cooled aeronautical combustor model (Q431846) (← links)
- Numerical simulation of effusion cooling with comparisons to experimental data (Q979559) (← links)
- Influence of intense surface cooling on hypersonic viscous flow past a delta wing (Q1304554) (← links)
- Tangential-slot film cooling on a plate in supersonic flow. Comparison of calculation and experiment (Q1402860) (← links)
- Two-dimensional Navier-Stokes solutions for transpiration cooling at hypersonic Mach numbers (Q1769888) (← links)