Control effectiveness and hinge-moment measurements at a Mach number of 1.9 of a nose flap and trailing-edge flap on a highly tapered low- aspect-ratio wing

Mitchell, Meade H , Jr Conner, D William
naca-rm-l8k17a
January 10, 1949


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1949/naca-rm-l8k17a.pdf