Fluidic Thrust Vectoring of Actively Controlled Nozzle Flows

L'abstract è presente nell'allegato / the abstract is in the attachment

Grantor dc:publisher

Politecnico di Torino

Year dc:date

2025

Author dc:creator

• RESTA, EMANUELE

Contributors dc:contributor

• FERLAUTO, MICHELE
• MARSILIO, Roberto

• Supersonic Nozzle
• FTV
• Shock Vector Control
• Differential Throttling
• Combustion
• Hot Flow
• Cold Flow
• Numerical Simulation
• CFD
• Experimental Test
• Pressure
• Mach
• Thrust Vectoring
• SSTO
• Aerospike
• Axisymmetric
• Linear
• Three Dimensional
• Grid Independence
• Turbulence Modeling
• RANS Equation
• Chemical Reaction
• Flowfield
• Characterization
• Settore IIND-01/G - Propulsione aerospaziale

Statement dc:rights

• info:eu-repo/semantics/openAccess
• license:Creative commons
• license uri:http://creativecommons.org/licenses/by-nc-nd/4.0/

Language dc:language

eng

Identifier

http://dx.doi.org/10.13121/polito/porto/3003995
10.13121/polito/porto/3003995

OAI identifier oai:identifier

oai:iris.polito.it:11583/3003995