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Publikováno v:
29th AIAA, Plasmadynamics and Lasers Conference.
Wind tunnel and flight tests have been used to investigate the vortex shedding characteristics of a low aspect ratio probe mount. Wind tunnel tests examined the nature of the flow at Mach 0.5, while flight tests examined the flow over Mach numbers ra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ee57a63aaf6dfc2065dc777154f2a698
https://doi.org/10.2514/6.1998-2831
https://doi.org/10.2514/6.1998-2831
