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Flight evaluation of the effects of leading-edge-slat span on the stability and control characteristics of a swept-wing fighter-type airplane during accelerated longitudinal maneuvers at transonic speeds
Document ID
19930089937
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Matranga, Gene J
Armistead, Katharine H
Date Acquired
August 29, 2013
Publication Date
March 6, 1958
Report/Patent Number
NACA-RM-H58A03a
Report Number: NACA-RM-H58A03a
Accession Number
93R19227
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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