Pages that link to "Item:Q4685472"
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The following pages link to Newly identified principle for aerodynamic heating in hypersonic flows (Q4685472):
Displaying 13 items.
- Mechanism of unsteady aerodynamic heating with sudden change in surface temperature (Q1016180) (← links)
- Influence of the velocity gradient on the stagnation point heating in hypersonic flow (Q1815771) (← links)
- An improved three-dimensional implicit discrete velocity method on unstructured meshes for all Knudsen number flows (Q2222450) (← links)
- Structure evolution at early stage of boundary-layer transition: simulation and experiment (Q4961082) (← links)
- A unified temperature transformation for high-Mach-number flows above adiabatic and isothermal walls (Q5049987) (← links)
- Theoretical and numerical study of the binary scaling law for electron distribution in thermochemical non-equilibrium flows under extremely high Mach number (Q5068965) (← links)
- Energy transfer structures associated with large-scale motions in a turbulent boundary layer (Q5144514) (← links)
- Dilatational-wave-induced aerodynamic cooling in transitional hypersonic boundary layers (Q5149503) (← links)
- On the Double-Step PIV Algorithm of Wall-Bounded Flows (Q5156674) (← links)
- Effect of a Tail with Non-Uniform Flexibility on Flapping Foil Dynamics (Q5156700) (← links)
- A metamorphosis of three-dimensional wave structure in transitional and turbulent boundary layers (Q5856554) (← links)
- Effect of flow–thermodynamics interactions on the stability of compressible boundary layers: insights from Helmholtz decomposition (Q6039572) (← links)
- Second-order analysis of hypersonic boundary-layer stability (Q6644875) (← links)
