Publication Date:
2016-06-07
Description:
To determine the feasibility of altering the formation and decay of aircraft trailing vortexes through aerodynamic means, the test capabilities of two wind tunnels and two towing basins were used. The facilities, common models, and measurement techniques that were employed in the evaluation of vortex minimization concepts are described.
Keywords:
AERODYNAMICS
Type:
Wake Vortex Minimization; p 129-156
Format:
application/pdf