Sidewash in the vicinity of lifting swept wings at supersonic speeds

Percy J. Bobbitt, Peter J. Maxie , Jr.
naca-tn-3938
Feb 1957


Equations and charts have been presented for the conical part of the sidewash above and below swept wings at small angles of attack. This flow-field component is necessary in making calculations of the wing-induced forces and moments on stores, missiles, and pylons. All supersonic Mach numbers and wing leading-edge sweep angles have been considered.

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