Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4

Knechtel, Earl D., Lee, George.
naca-rm-a57f06b
1957


Longitudinal aerodynamic characteristics at Mach numbers from 0.6 to 1.4 were measured to show the effect of drooping the outboard portions of wings having 53 degrees and 63 degrees of leading-edge sweep.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1957/naca-rm-a57f06b.pdf