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Effect of an Unswept Wing on the Contribution of Unswept-tail Configuration to the Low-speed Static and Rolling-stability Derivatives of a Midwing Airplane Model
Document ID
19930082786
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Letko, William
Riley, Donald R
Date Acquired
August 16, 2013
Publication Date
August 1, 1950
Report/Patent Number
NACA-TN-2175
Report Number: NACA-TN-2175
Accession Number
93R12076
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SIDEWASH
STABILITY, STATIC
INTERFERENCES - TAIL SURFACES & WING-FUSELAGE COMBINATION
TAIL SURFACE-WING COMBINATIONS
INTERFERENCE - TAIL SURFACES & WINGS
TAIL SURFACES, HORIZONTAL - POSITION
WIND TUNNEL TESTS - NACA - STABILITY
DOWNWASH
STABILITY, LATERAL

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