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The relationship of an integral wind shear hazard to aircraft performance limitationsThe development and certification of airborne forward-looking wind shear detection systems has required a hazard definition stated in terms of sensor observable wind field characteristics. This paper outlines the definition of the F-factor wind shear hazard index and an average F-factor quantity, calculated over a specified averaging interval, which may be used to judge an aircraft's potential performance loss due to a given wind shear field. A technique for estimating airplane energy changes during a wind shear encounter is presented and used to determine the wind shear intensity, as a function of the averaging interval, that presents significant hazard to transport category airplanes. The wind shear hazard levels are compared to averaged F-factor values at various averaging intervals for four actual wind shear encounters. Results indicate that averaging intervals of about one kilometer could be used in a simple method to discern hazardous shears.
Document ID
19940022090
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lewis, M. S.
(NASA Langley Research Center Hampton, VA, United States)
Robinson, P. A.
(NASA Langley Research Center Hampton, VA, United States)
Hinton, D. A.
(NASA Langley Research Center Hampton, VA, United States)
Bowles, R. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1994
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-109080
NAS 1.15:109080
Report Number: NASA-TM-109080
Report Number: NAS 1.15:109080
Accession Number
94N26593
Funding Number(s)
PROJECT: RTOP 505-64-12-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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