Experimental investigation of the effect of nozzle shape and test section perforation on the stationary and non-stationary characteristics of flow field in the large transonic TsAGI T-128 Wind tunnel

Publisher: Cambridge University Press

E-ISSN: 2059-6464|109|1092|75-82

ISSN: 0001-9240

Source: The Aeronautical Journal, Vol.109, Iss.1092, 2005-02, pp. : 75-82

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Abstract