The aerodynamic forces and moments on a one-tenth-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel

Ralph W. Stone, Jr., Sanger M. Burk, Jr., William Bihrle, Jr.
naca-tn-2181
Sep 1950


An investigation was conducted to provide general information on the magnitudes and directions of the aerodynamic forces and moments exerted on a model of a fighter airplane in spinning attitudes as measured on a rotary balance installed in the Langley 20-foot free- spinning tunnel.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1950/naca-tn-2181.pdf