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Experimental Determination of the Yawing Moment Due to Yawing Contributed by the Wing, Fuselage, and Vertical Tail of a Midwing Airplane Model
Document ID
19930092517
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mathews, Ward O
Date Acquired
September 6, 2013
Publication Date
June 1, 1943
Report/Patent Number
NACA-WR-L-387
NACA-ARR-3F28
Report Number: NACA-WR-L-387
Report Number: NACA-ARR-3F28
Accession Number
93R21807
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DRAG, PROFILE
MONOPLANES, MIDWING VS HIGH- & LOW-WING
STABILITY, LATERAL
YAWING MOMENTS - TAIL SURFACES
WINGS, HIGH-LIFT
YAWING MOMENTS - FUSELAGES
TAIL SURFACES, VERTICAL
WING FLAPS, SPLIT - PARTIAL-SPAN (20%-CHORD)
OSCILLATIONS
AIRFOILS - NACA 103

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