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Piloted-simulation evaluation of escape guidance for microburst wind shear encountersNumerous air carrier accidents and incidents result from encounters with the atmospheric wind shear associated with microburst phenomena, in some cases resulting in heavy loss of life. An important issue in current wind shear research is how to best manage aircraft performance during an inadvertent wind shear encounter. The goals of this study were to: (1) develop techniques and guidance for maximizing an aircraft's ability to recover from microburst encounters following takeoff, (2) develop an understanding of how theoretical predictions of wind shear recovery performance might be achieved in actual use, and (3) gain insight into the piloting factors associated with recovery from microburst encounters. Three recovery strategies were implemented and tested in piloted simulation. Results show that a recovery strategy based on flying a flight path angle schedule produces improved performance over constant pitch attitude or acceleration-based recovery techniques. The best recovery technique was initially counterintuitive to the pilots who participated in the study. Evidence was found to indicate that the techniques required for flight through the turbulent vortex of a microburst may differ from the techniques being developed using classical, nonturbulent microburst models.
Document ID
19890007449
Document Type
Thesis/Dissertation
Authors
Hinton, David A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1989
Subject Category
AIRCRAFT INSTRUMENTATION
Report/Patent Number
NASA-TP-2886
NAS 1.60:2886
DOT/FAA/DS-89/06
L-16498
Funding Number(s)
PROJECT: RTOP 505-66-41
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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