Actively cooled plate fin sandwich structural panels for hypersonic aircraft
1979
IX, 164 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Computational Design of Actively-Cooled Microvascular Composite Skin Panels for Hypersonic Aircraft
British Library Conference Proceedings | 2013
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