By Jim Sullivan
Booklet by means of Jim Sullivan, Dave Lucabaugh
Read Online or Download Golden wings, 1941-1945 : USN/USMC aircraft of World War II PDF
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Additional resources for Golden wings, 1941-1945 : USN/USMC aircraft of World War II
Example text
The process has a zero mean, that is, E[x] = 0. , independent of time). , ocean waves) every zero crossing from below is followed by a positive peak (crest), and every zero crossing from above is followed by a negative peak (trough). Therefore, the proportion of the positive zero crossings that also cross the level a with a positive slope represent the probability that the positive peak is larger than a, that is, P[ p > a] = 1 − P[ p ≤ a] = 1 − F p (a) = νa+ νo+ (29) where F p (a) is the cumulative distribution function (CDF) of the peak values.
In many regions of the ocean, a three-parameter Weibull distribution offers a better fit than the two- e−[(x−m)/k] (59) where the new parameter, m, is the location parameter. All three parameters are to be determined from wave statistics in any ocean zone using, for example, regression analysis. Another basic assumption in the preceding analysis of loads on ships is the linearity assumption. In high seas, this assumption is violated and the difference between sagging and hogging moments, which is not recognized by the linear theory, becomes important.
SWAN (see Sclavounos 1996; Sclavounos et al. 1997) is also a multilevel motions and loads computer program suite. It solves the hydrodynamic problem similar to LAMP using the Rankine source. Both SWAN and LAMP have been validated to some extent with model test data. Shin et al. (1997) further compares the measured frequency response functions (FRF) for heave, pitch, roll, and vertical and horizontal bending moments amidships of the S175 container ship, with two numerical calculations labeled by ABS-SM and LAMP-1, as shown in Fig.