Zobrazeno 1 - 2
of 2
pro vyhledávání: '"Soumya R. Nanda"'
Publikováno v:
25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Publikováno v:
Experiments in Fluids. 64
Hypersonic leading-edge separation is studied towards understanding the varying shock-related unsteadiness with freestream Reynolds number ($1.66 \times 10^5 \leq Re_D \leq 5.85 \times 10^5$) in the newly constructed hypersonic Ludwieg tunnel (HLT) a