Wake vortex encounter hazards criteria for two aircraft classes

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

An investigation was conducted using a piloted, motion-base simulator to determine wake vortex hazard criteria for two classes of jet transport aircraft. A light business jet and a large multiengine jet transport were represented respectively. The hazard boundaries were determined in terms of the maximum bank angle due to the vortex encounter. Upsets as small as 7 deg in bank angle were considered to be hazardous at breakout altitude (200 ft (61.0 m)) for Instrument Flight Rule (IFR) and at 50 ft (15.2 m) for Visual Flight Rule (VFR) for both aircraft classes. Proximity to the ground was the primary reason for a hazardous rating. This was reflected in the reduction in the maximum bank angle at the hazard boundary and in more consistent ratings as altitude was decreased.

Authors

• Sammonds, R. I. NASA Ames Research Center
• Stinnett, G. W., Jr. NASA Ames Research Center
• Larsen, W. E. FAA