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Influence of large amounts of wing sweep on stability and control problems of aircraft
Document ID
19930081707
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Soule, Hartley A
Date Acquired
August 29, 2013
Publication Date
June 1, 1946
Report/Patent Number
NACA-TN-1088
Report Number: NACA-TN-1088
Accession Number
93R10997
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIR FLOW VELOCITY, HIGH - SUBSONIC
WINGS - DIHEDRAL
WINGS - SWEEPBACK
WINGS - SWEEPBACK & SWEEPFORWARD
STABILITY & CONTROL
AIRFOILS - NACA 23012 - CHAR & MOMENTS WING FLAPS, SPLIT
LANDING SPEED
AIRFOILS - NACA 23012 - CHAR & MOMENTS

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