Mach number distribution for subsonic flow over a bump.
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PPT - Techniques for High-order Adaptive Discontinuous Galerkin Discretizations in Fluid Dynamics Dissertation Defense PowerPoint Presentation - ID:6622
Out-of-plane deflection at blade tip for an inflow velocity of 50 m s .
A physical explanation for the formation of shocks in transonic flow. ( Description in the comments) : r/TurbineEngines
Flow instabilities and impact of ramp–isolator junction on shock–boundary-layer interactions in a supersonic intake, Journal of Fluid Mechanics
Sketch of scour downstream of an apron.
Locations denoted by A and B at which near-field spectra
Spanwise distribution of pitch averaged loss coefficient ζ, comparison
Subsonic Flow - an overview
Ch9 Linearized Flow 9.1 Introduction - ppt download
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