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 24
NACA RM L52B13 23 … *1 Figure 10.- Variation of pressure-rise ratio with vortex generators over a range of inlet-houndary-layer displacement thickness = 2.85; = 7.3; £ = 0.5; a = 15° 5*-,
NASA Technical Reports Server (NTRS)
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