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Fig. 4. Contour plots of thrust coefficient for
h0/c=1.0 (A) and h0/c=1.5
(B); max is given in degrees. Red circles represent location
of each run performed; no data exist for the region shadowed in grey for
h0/c=1.0.
max is given in degrees. Red circles represent location
of each run performed; no data exist for the region shadowed in grey for
h0/c=1.0.