Effects of Some Primary Variables of Rectangular Vortex Generators on the Static-pressure Rise Through a Short Diffuser (1952)
NASA Technical Reports Server (NTRS) · leaf 33
NACA RM L52B13 32 … dl Figure 17.- Pressure-rise ratio with the selected vortex generators for a range of inlet-houndary-layer-displacement thickness d = 2.09; £ = o.327; a = 15°). NACA-Langley - 5-2-55 - 75
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
