Which risk increases when transitioning to supersonic speeds?

💡 Explanation

Compressor stall risk increases because the **boundary layer separation** turbulence induces flow distortions. This reduces the compressor's ability to deliver compressed air, leading to stall at lower pressure ratios; therefore, stall probability increases rather than decreased efficiency or stress under these conditions.

• Which mechanism causes increased electron tunneling across semiconductor interfaces in strained silicon MOSFETs?
• Which consequence results when electrons violate the Pauli exclusion principle within a white dwarf star?
• Which outcome occurs when a pump impeller operates significantly below its optimal Reynolds number?
• Which temperature profile inhibits power output when optimizing a Carnot heat engine?
• Which outcome occurs when pressure exceeds supercritical fluid threshold?
• Which outcome occurs when a transformer operates far above rated frequency?