Pages that link to "Item:Q3537507"
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The following pages link to Disturbance evolution in the leading-edge region of a blunt flat plate in supersonic flow (Q3537507):
Displaying 3 items.
- Fluid mechanics research at the Institute of Aerodynamics, RWTH Aachen University: from 1912 through 2012 (Q1670026) (← links)
- Stochastic boundary condition effects on supersonic leading edge blowing (Q2158170) (← links)
- On high-order shock-fitting and front-tracking schemes for numerical simulation of shock-disturbance interactions (Q2638216) (← links)