Application to airfoils of a technique for reducing orifice-induced pressure error at high reynolds numbers
Application to airfoils of a technique for reducing orifice-induced pressure error at high reynolds numbers
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- Washington, D.C. National Aeronautics and Space Administration 1986
- 42 p.
- NASA TP 2537 : 1986 .
Pressure measurement, Static pressure, Orifices,Errors, Porous materials
LNASA TP 2537 : 1986
Pressure measurement, Static pressure, Orifices,Errors, Porous materials
LNASA TP 2537 : 1986