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Theoretical supersonic lift and drag characteristics of symmetrical wedge-shape-airfoil sections as affected by sweepback outside the Mach coneThe theoretical supersonic section lift and drag characteristics of thin wedge-shape, untapered airfoils with sweepback are presented. The results apply to those parts of the wing in two dimensional flow and are not applicable to wings swept back within the Mach cone of the center section. The results may also be applied to swept-forward wings if the angle of sweep is not enough to put the wing within the Mach cone from the tips.
Document ID
19930081841
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ivey, H Reese
Bowen, Edward N , Jr
Date Acquired
August 16, 2013
Publication Date
March 1, 1947
Report/Patent Number
NACA-TN-1226
Report Number: NACA-TN-1226
Accession Number
93R11131
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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