Table 6 Summary of flow conditions for hypersonic experimental data.

Flat plate

Ma = 6, Re = 9.7 × 10⁶/m

T_0,∞ = 464 K, P_0,∞ = 1Mpa, T_w~300 K

Ma = 6, Re = 1.94 × 10⁷/m

T_0,∞ = 464 K, P_0,∞ = 2Mpa, T_w~300 K

Blunt cone

Ma = 4.94, Re = 2.17 × 10⁷/m,

T_0,∞ = 363 K, P_0,∞ = 1Mpa, T_w~300 K,

β = 7°, SR = 2.5/5 mm, α = 0°

Ma = 6.97, Re = 1.5 × 10⁷/m,

T_0,∞ = 600 K, P_0,∞ = 3.5Mpa, T_w~300 K,

β = 7°, SR = 1.6 mm, α = 0/3/5/7°

Compression corner

Ma = 4.955, Re = 4.4 × 10⁷/m,

T_0,∞ = 373 K, P_0,∞ = 2Mpa, T_w~300 K, β = 34°

Ma = 5.93, Re = 0.9754 × 10⁷/m,

T_0,∞ = 464 K, P_0,∞ = 1Mpa, T_w~300 K, β = 34°