Shock tube study on the disintegration of fuel jets at elevated pressures and temperatures
1. Aufl.
2011
XX, 196 S.
210 mm x 148 mm, 343 g
Ill., graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Digital preservation by Universitätsbibliothek Stuttgart
Theses
English
BKL: | 52.30 Strömungskraftmaschinen, Turbomaschinen |
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