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Analog study of the longitudinal response of a swept-wing transport airplane to wind shear and sustained gusts during landing approachAnalog computed time histories and altitude-ground track plots of swept wing transport aircraft longitudinal response to wind shear and sustained gusts during landing approaches
Document ID
19680009711
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Snyder, C. T. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4477
Accession Number
68N19180
Funding Number(s)
CONTRACT_GRANT: 126-16-05-07-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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