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Wind-tunnel Tests at Low Speed of Swept and Yawed Wings Having Various Plan FormsResults are presented of wind-tunnel tests made at low speed of various small-scale models of sweptback, sweptforward, and yawed wings. The tests covered changes in aspect ratio, taper ratio, and tip shape. Some data were obtained with high-lift devices on sweptback wings and with ailerons on sweptforward wings. The data have been briefly analyzed and some comparisons have been made with the available theory.
Document ID
19930083063
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Purser, Paul E
Spearman, M Leroy
Date Acquired
August 16, 2013
Publication Date
December 1, 1951
Report/Patent Number
NACA-TN-2445
Report Number: NACA-TN-2445
Accession Number
93R12353
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HIGH LIFT DEVICES - COMPLETE WINGS
WINGS, COMPLETE - SWEEP
WINGS, COMPLETE - DESIGN VARIABLES

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