| | Concept to Reality |
 | | The coordinated research program performed at the centers investigated the effectiveness of a myriad of aerodynamic schemes such as spoilers, vortex generators, wingtip vortex-attenuating devices, steady and pulsed mass injection, oscillating control inputs, and span load variations. |
 | | After extensive parameter variations in the VRF and in-flight assessments with the C-54 as a generating aircraft and a Piper PA-28 general aviation aircraft as a probe aircraft, the researchers concluded that the spline device was effective in reducing the strength of the trailing vortex. |
 | | The vortex attenuation achieved in flight was greater than that obtained in the VRF, and the researchers anticipated that the installation of stowable spline devices on commercial jet aircraft would avoid the obvious penalties in climb capability in the landing phase of flight and increased approach noise due to increased power settings. |
| oea.larc.nasa.gov /PAIS/Concept2Reality/wake_vortex.html (8008 words) |