| 摘要 |
<p>Retarding of the point of transition (3) from laminar flow (2) to turbulent flow (4) in aerodynamic boundary layers on the surfaces (1) of aircraft is accomplished by radiating acoustic energy at frequencies greater than twice the critical Tollmein-Schlichting frequency into the boundary layer. The acoustic energy interferes with the formation of Tollmein-Schlichting waves, thereby increasing the incidence of laminar flow and reducing aerodynamic drag.</p> |
