Comparative tests of the rolling effectiveness of constant-chord, full-delta, and half-delta ailerons on delta wings at transonic and supersonic speeds

Carl A. Sandahl, H. Kurt Strass
naca-rm-l9j26
Dec 1949


Comparative tests of the rolling power of plain constant-chord, full-delta, and half-delta ailerons on delta wings having 45 and 60 degree leading-edge sweepback have been made utilizing rocket-propelled test vehicles in free flight.

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http://naca.central.cranfield.ac.uk/reports/1949/naca-rm-l9j26.pdf