Effects of Reynolds Number on Flow over 76/40-Degree Double-Delta Wings

摘要

The effects of the Reynolds number on the flow over 76/40-deg double-delta or strake-wing configurations and the capability of numerical solutions to predict these effects are discussed. The flow over the strake appears to be little affected by the Reynolds number. On the wing strong effects are evident on the flow on and off the wing surface. Numerical solutions tend to reasonably well predict the flow over these types of configurations.