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Approximate relations and charts for low-speed stability derivatives of swept wingsContains derivations, based on a simplified theory, of approximate relations for low-speed stability derivatives of swept wings. Method accounts for the effects and, in most cases, taper ratio. Charts, based on the derived relations, are presented for the stability derivatives of untapered swept wings. Calculated values of the derivatives are compared with experimental results.
Document ID
19930082233
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Toll, Thomas A
Queijo, M J
Date Acquired
August 16, 2013
Publication Date
May 1, 1948
Report/Patent Number
NACA-TN-1581
Report Number: NACA-TN-1581
Accession Number
93R11523
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THEORIES - WINGS SWEPTBACK & SWEPTFORWARD
STABILITY CALCULATIONS
AIRFOILS - ASPECT RATIO, SMALL
AIRFOILS - NACA 0012
WINGS, SWEPTBACK & SWEPTFORWARD - STABILITY
SIDESLIPPING
EQUATIONS - STABILITY
ROLLING, PITCHING & YAWING MOMENTS - WINGS
CHARTS - STABILITY
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