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I challenge the assertion that "ram pressure" can only exist during supersonic flow. I would define "ram pressure" to be equivalent to the dynamic pressure of the flow, equal to (1/2) x (density) x (velocity)^2 in the incompressible regime, and defined by the total pressure/static pressure compressible relation in the compressible regime (Ma > 0.3). - Fyre4ce
I challenge the assertion that "ram pressure" can only exist during supersonic flow. I would define "ram pressure" to be equivalent to the dynamic pressure of the flow, equal to (1/2) x (density) x (velocity)^2 in the incompressible regime, and defined by the total pressure/static pressure compressible relation in the compressible regime (Ma > 0.3). - Fyre4ce

:Not a Physics student here. Just to add this: if any body can pressure any fluid, then the concept of ram pressure is strongly connected to the one of buoyancy, isn't it right? This should be mentioned and further explained in the main article, if my observation is correct.

Revision as of 22:44, 29 December 2006

I challenge the assertion that "ram pressure" can only exist during supersonic flow. I would define "ram pressure" to be equivalent to the dynamic pressure of the flow, equal to (1/2) x (density) x (velocity)^2 in the incompressible regime, and defined by the total pressure/static pressure compressible relation in the compressible regime (Ma > 0.3). - Fyre4ce

Not a Physics student here. Just to add this: if any body can pressure any fluid, then the concept of ram pressure is strongly connected to the one of buoyancy, isn't it right? This should be mentioned and further explained in the main article, if my observation is correct.