Measurements of Flow in the Boundary Layer of a 1/40-Scale Model of the U. S. Airship "Akron." (1933)
NASA Technical Reports Server (NTRS) · leaf 8
ent (approximate) The method of derivation of this equation is similar to Position 8 that used by Von Karman (reference 10, see also refer- 0 JO .20 .30 .40 .50 .60 .70 .80 .90 1.00 y/s i.o Kigukk .r>.—Velocity distribution for laminar and turbulent portions of boundary layer—airship model Akron 0.… … 0.0/ 0.02 0.04 0.08 .1 0.2 0.4 0.6 0.8 I. against the distance x and the resulting curves are y/<5 designated A and B. These curves are differentiated Figure 6.—Logarithmic plot of velocity distribution—airship model Akron graphically and the equation solved for the frictional the variation of the…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
