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  1. Freestream Effects on Boundary Layer Disturbances for HIFiRE-5
  2. Low-temperature collisional quenching of NO A2Σ+(v′ = 0) by NO(X2Π) and O2 between 34 and 109 K
  3. Effect of a Normal Shock Wave on Freestream Total Pressure Fluctuations in a Low-Density Mach 6 Flow