Point drag and total drag of navy struts no. 1 modified (1923)
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sure along the section. The values so computed are given in figure 8. The agreement between the calculated and observed values is close for the foremost holes, but more or less" divergent for the holes farther aft in the part of the surface before the major section. This discrepancy was caused, no… … Air speed' V(mji.h) Fio. 6.—Observed pressure" vs. velocity at rero pitch and Fra. 9.—Resistance and shape coefficients tor Navy struts Nos. 2 and 3. yaw for Navy stmt No. 2. tion over the spheroidal bow of a torpedo form, given in Report No. 600 of the British Advisory Committee for Aeronautics…
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