Experimental study of bluntness effect on hypersonic boundary-layer transition over slender cone using surface mounted pressure sensors

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  • who: Ranran Huang from the School of Aerospace University of Science People`s Republic of China have published the Article: Experimental study of bluntness effect on hypersonic boundary-layer transition over slender cone using surface mounted pressure sensors, in the Journal: (JOURNAL)
  • what: In this work, the bicoherence is calculated from time-series data using a Hamming window with 50% overlap, and the points of each window are 1024. The authors investigated the influence of nose tip bluntness on the hypersonic boundary-layer transition in a noisy Ludwieg tube tunnel with the aid of surface . . .

     

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