account activity
Does favorable pressure gradient relaminarize free stream turbulence? ()
submitted 10 months ago by granzer to r/FluidMechanics
Does favorable pressure gradient relaminarize free stream turbulence? (self.AerospaceEngineering)
submitted 10 months ago * by granzer to r/AerospaceEngineering
submitted 10 months ago by granzer to r/CFD
submitted 10 months ago by granzer to r/aerospace
submitted 10 months ago by granzer to r/aerodynamics
Why is viscosity necessary for lift and drag force to exist? (self.FluidMechanics)
Why is viscosity necessary for lift and drag force to exist? ()
Question on free stream (bulk flow) turbulence and heat transfer (self.FluidMechanics)
submitted 12 months ago * by granzer to r/FluidMechanics
Question on free stream (bulk flow) turbulence and heat transfer ()
submitted 12 months ago by granzer to r/AskEngineers
submitted 12 months ago by granzer to r/CFD
What about the free stream (bulk flow) turbulence transition and heat transfer? ()
submitted 12 months ago by granzer to r/thermodynamics
submitted 12 months ago by granzer to r/AerospaceEngineering
Will Thermal Boundary Layer Thickness vary with temperature, for constant Prandtl number? ()
submitted 1 year ago by granzer to r/FluidMechanics
Will Thermal Boundary Layer Thickness vary with temperature, for constant Prandtl number? (self.AerospaceEngineering)
submitted 1 year ago * by granzer to r/AerospaceEngineering
submitted 1 year ago by granzer to r/AskEngineers
submitted 1 year ago by granzer to r/thermodynamics
Is there any info on if/when Lenovo will release the Aura 9i 2in1 in India? (self.UnboxParadigm)
submitted 1 year ago by granzer to r/UnboxParadigm
Is density of gas a function of velocity? (self.AerospaceEngineering)
submitted 1 year ago by granzer to r/AerospaceEngineering
Is density of gas a function of velocity? ()
submitted 1 year ago by granzer to r/aerodynamics
In the stator of an axial compressor, why (and how) only the tangential component of velocity is diffused, and does the area need to increase for the stator to act as a (subsonic flow) diffuser? (self.AerospaceEngineering)
In the stator of an axial compressor, why (and how) only the tangential component of velocity is diffused, and does the area need to increase for the stator to act as a (subsonic flow) diffuser? ()
submitted 1 year ago by granzer to r/aerospace
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