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Investigation at Low Speed of the Longitudinal Stability Characteristics of a 60 Degree Swept-back Tapered Low-drag Wing
Document ID
19930081900
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lowry, John G
Schneiter, Leslie E
Date Acquired
August 16, 2013
Publication Date
May 1, 1947
Report/Patent Number
NACA-TN-1284
Report Number: NACA-TN-1284
Accession Number
93R11190
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - NAVY N-22 - CHAR , A C & MOMENTS WING SLOTS & FLAPS
WING FLAPS, LEADING-EDGE
AIRFOILS - NACA 65-210 - CHAR , A C & MOMENTS LOW-DRAG
STABILITY, LONGITUDINAL
WING TIP SLOTS
WIND TUNNEL TESTS - NACA - 300 MPH WORK CARRIED ON AT LMAL
WINGS, SWEPTBACK - STABILITY, LONGITUDINAL
AIRFOILS - ASPECT RATIO
WING TIPS, EXTENDED

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