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J-GLOBAL ID:200902177205919804
整理番号:93A0548904
Coupled electrical and thermal transfers in a glass-epoxy carbon composite. Application to the design of a helicopter blade de-icer.
Transferts electriques et thermiques couples dans un materiau composite carbone-verre epoxy. Application a la realisation d’un degivreur de pale d’helicoptere.
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