Drone impact assessment on aircraft structure: windshield and leading edge testing and analysis

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DOIResolve DOI: https://doi.org/10.4224/40001907
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  1. National Research Council of Canada. Aerospace
FormatText, Technical Report
Physical descriptionvolume 2 of 2, 58 p.
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PublisherNational Research Council of Canada. Aerospace Research Centre
LanguageEnglish
Peer reviewedNo
IdentifierCR-GTL-2020-0054
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Record identifier28f1d264-a3c2-449b-bbc1-39747f58e632
Record created2020-09-28
Record modified2020-10-06
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