Burn-Through Responses of Aero-Engine Nacelle using Fiber Metal Composites by ISO2685 Propane-Air Burner
Crossref DOI link: https://doi.org/10.35940/ijrte.D9224.118419
Published Online: 2019-11-30
Update policy: https://doi.org/10.35940/beiesp.crossmarkpolicy
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Mohammed*, Ibrahim
Talib, Abd Rahim Abu
