10 citations · 23 across the 5 of their papers we have counts for
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S. K. Karthick, Soumya R. Nanda, J. Cohen
Hypersonic leading-edge separation is studied towards understanding the varying shock-related unsteadiness with freestream Reynolds number ($1.66 \times 10^5 \leq Re_D \leq 5.85 \t…