导航
ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1996, Vol. 17 ›› Issue (S1): 114-116.
• 论文 • Previous Articles Next Articles
Yao Jin
Received:
Revised:
Online:
Published:
Abstract: The general approach to sonic fatigue test spectrum was discussed at first. A special method based on the measured acoustic data and analysed by one octave band or one third octave band analyser was introduced here. The method was successfully applied to actual sonic fatigue tests.
Key words: sonic fatigue, test spectrum, data generations
CLC Number:
V215. 5
Yao Jin. A METHOD FOR DEVELOPING SONIC FATIGUE TEST SPECTRUM OF AIRCRAFT STRUCTURE[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(S1): 114-116.
0 / / Recommend
Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks
URL: https://hkxb.buaa.edu.cn/EN/
https://hkxb.buaa.edu.cn/EN/Y1996/V17/IS1/114
CJA
