Wind-tunnel investigation at high subsonic speeds to determine the rolling derivatives of two wing-fuselage combinations having triangular wings, including a semiempirical method of estimating the rolling derivatives

Wiggins, James W
naca-rm-l53l18a
February 08, 1954


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1954/naca-rm-l53l18a.pdf