N.A.C.A. Technical Memorandum No.519 Figs.6,7,12,17. •400 CQ h200 B Eh 0 100 200 300 .4 .6 V/Dn Graduations on instrument Fig.6 Thrust-measuring hub Fig.7 Thrust coefficients (calibration curve). measured in flight. 120 100 bo M s 80 (D g. 60 u o ** 40 20 0 0 20 .40 60 80 Graduations on instrument… … Fig.17 Representation of a test installation for full- size float and hull investigations.
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