Advances in Aerodynamics

Table 1 Back pressure conditions

From: Flow field reconstruction and shock train leading edge position detection of scramjet isolation section based on a small amount of CFD data

Number	A (Pa)	B (Pa)	f (Hz)
1	61,740	4410	100
2	66,150	4410	100
3	70,560	4410	100
4	74,970	4410	100
5	79,380	4410	100

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