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Static stability characteristics at Mach numbers from 1.90 to 4.63 of a 76 deg swept arrow wing model with variations in horizontal-tail height, wing height, and dihedralHorizontal-tail height, wing height, and dihedral effects on longitudinal and lateral stability characteristics of 76 deg swept arrow wing aircraft model
Document ID
19670024546
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Fuller, D. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-4076
Report Number: NASA-TN-D-4076
Accession Number
67N33875
Funding Number(s)
CONTRACT_GRANT: 126-13-02-04-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DIHEDRAL EFFECT
AIRCRAFT MODEL
STATIC STABILITY
HORIZONTAL TAIL
ARROW WING

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