Summary of some effective aerodynamic twisting-moment coefficients of various wing-control configurations at Mach numbers from 0.6 to 1.7 as determined from rocket-powered models

H. Kurt Strass
naca-rm-l51k20
Jan 1952


A summary is presented of some effective aerodynamic twisting-moment coefficients of various wing-control configurations for use at Mach numbers from 0.6 to 1.7 as determined by the Langley Pilotless Aircraft Research Division by the use of rocket-propelled models. The values thus obtained were determined by the combined use of the experimentally determined free-flight data and subsonic aerodynamic theory.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1952/naca-rm-l51k20.pdf