JOURNEY IN AERONAUTICAL
RESEARCH: A Career at NASA Langley Research Center
Monographs in
Aerospace History, Number 12
FIGURE 11.3. Typical data wing-flow
test. Plot of flap hinge moment as a function of angle of attack at
various values of Mach number, gap sealed and unsealed.
(a) Mach number from 0.65 to 1.15 in
steps of 0.05.
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