Theoretical Analysis of a Gust Alleviator Used on a Lancaster Aircraft and Comparison with Experiment
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Communicated by the Principal Director of Scientific Research (air), Ministry of Supply
Imomlbressibte Flow Summary.-The report presents the theoretical calculations of gust alleviation factor made for rigid aircraft and with one degree of freedom only (i.e., vertical motion). It is shown that for average gust lengths and for orthodox (tailed) aircraft the influence of thesecond degree of freedom (i.e., pitching) on the value of the gust alleviation factor is negligibly small, pro...
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تاریخ انتشار 2002