Free-flight investigation at transonic and supersonic speeds of the rolling effectiveness of a thin, unswept wing having partial-span ailerons

Carl A. Sandahl
naca-rm-l8g20a
Oct 1948


An investigation of the rolling effectiveness at transonic and supersonic speeds of a thin, unswept wing having partial-span ailerons has been made by means of rocket-propelled test vehicles.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1948/naca-rm-l8g20a.pdf