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1 Ergebnisse
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Design of Hypersonic Scramjet Engine Operating between Mach..:
, In:
2019 Sixth International Conference on Aerospace Science and Engineering (ICASE)
,
Khan, Daniyal Ahmed
;
Hassan, M. Hammad
;
Qamar, Ihtzaz
- p. 1-6 , 2019
Link:
https://doi.org/10.1109/ICASE48783.2019.9059159
RT T1
2019 Sixth International Conference on Aerospace Science and Engineering (ICASE)
: T1
Design of Hypersonic Scramjet Engine Operating between Mach 5 to Mach 9
UL https://suche.suub.uni-bremen.de/peid=ieee-9059159&Exemplar=1&LAN=DE A1 Khan, Daniyal Ahmed A1 Hassan, M. Hammad A1 Qamar, Ihtzaz YR 2019 K1 Fuels K1 Isolators K1 Engines K1 Electric shock K1 Combustion K1 Geometry K1 Hydrogen K1 hypersonic K1 scramjet K1 propulsion K1 supersonic combustion K1 stream thrust analysis SP 1 OP 6 LK http://dx.doi.org/https://doi.org/10.1109/ICASE48783.2019.9059159 DO https://doi.org/10.1109/ICASE48783.2019.9059159 SF ELIB - SuUB Bremen
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