B-25 航空エンジンの高空動特性取得試験(開発・性能II,一般講演)

概要

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The dynamic response characteristics of single spool turbojet engine under the high altitude flight condition were acquired from the frequency responses and step responses tests of the real engine at the altitude test facility. Also, the transfer functions were estimated by the analytical method, and verified by comparing with the frequency characteristics of the real engine. Furthermore, it made possible that the dynamic characteristics under any flight envelop could be estimated from the corrected formed transfer functions.
公益社団法人日本ガスタービン学会の論文
2006-10-01