Publikationsdatum:
2019-06-28
Beschreibung:
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings of aspect ratios 2 and 4 at Mach numbers of 1.45 and 1.97. The investigation includes some comparison of the effects of Reynolds number and of thickening the wing root sections on the loading.
Materialart:
NACA-RM-A54D19
Format:
application/pdf