Publication Date:
2019-06-28
Description:
The flow around a hemisphere-cylinder was studied at angles of attack alpha = 0-90 deg. The work was carried out in two wind tunnels, using hot wire anemometers and seven-hole probes at Reynolds number of 2.7 x 10 exp 4. Five distinct states of vortex unsteadiness were detected. For angles of attack less than 14 deg, the flow is rather stable. For alpha between 15 and 23 deg, meandering occurs at a reduced frequency of 0.065. For alpha between 24 and 32 deg, three frequencies were recorded at 0.11, 0.21, and 0.31. At even higher angles of attack, alpha between 33 and 41 deg, two frequencies were seen at 0.11 and 0.19. The onset of alternate shedding is at alpha = 42 deg, above which, alternate shedding occurred at 0.065. However, above 55 deg, shedding occurred at 0.15. Asymmetric wake structures over the hemisphere-cylinder were also investigated. It was found that asymmetric structures too are not steady but engage in periodic organized motions.
Keywords:
AERODYNAMICS
Type:
AIAA PAPER 91-3268
Format:
text
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