Fluidic Thrust Vectoring of Actively Controlled Nozzle Flows
type: CreativeWork
description: L'abstract è presente nell'allegato / the abstract is in the attachment
abstract: L'abstract è presente nell'allegato / the abstract is in the attachment
author: RESTA, EMANUELE
language: eng
keywords: 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
date published: 2025-09-16
date modified: 2026-07-24T03:50:50Z
provider: Politecnico di Torino
publisher: Networked Digital Library of Theses and Dissertations
type: WebPage
source organization: Politecnico di Torino

PropertyValue
property ID: Handle
value: https://hdl.handle.net/11583/3003995

PropertyValue
property ID: DOI
value: 10.13121/polito/porto/3003995