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Experimental aerodynamic investigations of the NASA Common Research Model have been conducted in the NASA Langley National Transonic Facility, the NASA Ames 11-ft wind tunnel, and the European Transonic Wind Tunnel. In the NASA Ames 11-ft wind tunnel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::018038947daec2c7cf8968f6cfba57fa
https://elib.dlr.de/95284/
https://elib.dlr.de/95284/
Publikováno v:
Experiments in Fluids. 28:477-481
Density fields of the blade tip vortices from a helicopter in hover flight were visualized by a technique which does not require any installation on the helicopter or close to it. The results illustrate an encouraging prospect for the applicability o