Table 2 Wind tunnel operating parameters
From: Hypersonic aerodynamic force balance using temperature compensated semiconductor strain gauges
Ma | T0 (K) | P0 (MPa) | Re (× 105) | AoA (°) | Flow medium |
|---|---|---|---|---|---|
12.7 | 600 | 2.0 | 4.44 | −4° ~ 8° | N2 |
From: Hypersonic aerodynamic force balance using temperature compensated semiconductor strain gauges
Ma | T0 (K) | P0 (MPa) | Re (× 105) | AoA (°) | Flow medium |
|---|---|---|---|---|---|
12.7 | 600 | 2.0 | 4.44 | −4° ~ 8° | N2 |