Hinge-moment and effectiveness characteristics of an aspect-ratio-8.2 flap-type control on a 60 degree delta wing at Mach numbers from 0.72 to 1.96

Guy, Lawrence D
naca-rm-l56j17
January 07, 1957


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1957/naca-rm-l56j17.pdf