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Effects of Supersonic Nozzle Geometry on Characteristics of Shock Wave Structure

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Figure

Figure 1. Experimental apparatus.
Figure 2. Nozzle geometry.
Figure 4. Schlieren photographs. (a) BN; (b) EN-11; (c) EN-55; (d) ND-0.2; (e) ND-1.0; (f) NU-0.2; (g) NU-1.0
Figure 8. Distance from triple point to upper and lowalls (BN, NU-0.2, NU-1.0). wer

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