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Numerical investigation on non-premixed combustion in a typical film cooled cryogenic rocket thrust chamber

By:

Madhusoodanan Pillai,K

Material type: Text

Text

TextPublication details: TVPM Comptational fluid dynamics laboratory,University of Kerala 2017Other classification:

D646-58,7:(c217):f

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Holdings
Item type	Current library	Home library	Collection	Call number	Status	Date due	Barcode
PhD Thesis	Kerala University Library Reference	Kerala University Library	Thesis	D646-58,7:(c217):f Q7(RT) (Browse shelf(Opens below))	Not for loan		G41173

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Previous	D62,75:(B2881) Q7(RT) Swarm intelligence based algorithms for multi objective optimization	D62,75:(C7) Q6(RT) Design,modeling and characterization of magneto-rhelogical dampers	D64121:(D587) Q7(RT) An investigation on composite throat inserts for model thrust chamber of liquid rocket engine	D646-58,7:(c217):f Q7(RT) Numerical investigation on non-premixed combustion in a typical film cooled cryogenic rocket thrust chamber	D6468,8(D5,7):81 Q5(RT) Investigation on the effect of thrust chamber geometric parameters on the performance of NTO/MMH thrusters	D6513:33:b2 Q6(RT) An investigation into modelling complex systems using constrained objects	D6513:33UML:(B61) Q6(RT) On the specifications of sequence constraints in UML	Next

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