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Table 8 Trial and error related to the blank pressure change between two phases and variations of the logarithmic strain

From: Simulated and experimental investigation of the airfoil contour forming of 301 austenitic stainless steel considering the springback

Test number

Pressure of phase 1 (Mpa)

Pressure of phase 2 (Mpa)

Logarithmic strain (%)

1

0.163

0.163

10.5753

2

0.163

0.2445

9.3986

3

0.163

0.3667

9.2097

4

0.163

0.5501

9.9174

5

0.163

0.8252

9.5038

6

0.163

1.2377

9.0166

7

0.163

1.8565

8.3665

8

0.163

2.7848

8.7862