Francesco Nasuti | Ricerc@Sapienza

Publications

Title	Published on	Year
Low order investigation on longitudinal combustion instability in a variable geometry single element combustor	7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS)	2017
Delayed detached eddy simulation of separated ﬂows in a planar nozzle	7TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS)	2017
Modeling of high density polyethylene regression rate in the simulation of hybrid rocket flowﬁelds	7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS)	2017
Evolution of cooling-channel properties for varying aspect ratio	PROGRESS IN PROPULSION PHYSICS	2016
Experimental investigation of transcritical methane flow in rocket engine cooling channel	APPLIED THERMAL ENGINEERING	2016
Chemical reaction effects on heat loads of CH4/O2 and H2/O2 rockets	AIAA JOURNAL	2016
Hybrid rockets with axial injector: port diameter effect on fuel regression rate	JOURNAL OF PROPULSION AND POWER	2016
Modeling of paraffin-based fuels in the simulation of hybrid rocket flowfields	52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016	2016
Validation of conjugate heat transfer model for rocket cooling with supercritical methane	JOURNAL OF PROPULSION AND POWER	2016
Moretti's shock-fitting methods on structured and unstructured meshes	Handbook of mumerical methods for hyperbolic problems. Basic and fundamental issues	2016
Heat transfer modeling for supercritical methane flowing in rocket engine cooling channels	APPLIED THERMAL ENGINEERING	2015
Navier–Stokes simulation of graphite nozzle erosion at different pressure conditions	AIAA JOURNAL	2015
Radius of curvature effects on throat thermochemical erosion in solid rocket motors	JOURNAL OF SPACECRAFT AND ROCKETS	2015
Simulation of gaseous oxygen/hydroxyl-terminated polybutadiene hybrid rocket flowfields and comparison with experiments	JOURNAL OF PROPULSION AND POWER	2015
Convective and radiative contributions to wall heat transfer in liquid rocket Engine thrust chambers	51st AIAA/ASME/SAE/ASEE Joint Propulsion Conference	2015
Numerical analysis of port diameter effect on hybrid rocket fuel regression rate with axial injection	51st AIAA/SAE/ASEE Joint Propulsion Conference - Proceedings	2015
Determination of heat release response function from 2D hybrid RANS-LES data for the CVRC combustor	51st AIAA/SAE/ASEE Joint Propulsion Conference - Proceedings	2015
Response function modeling in the study of longitudinal combustion instability by a quasi-1D eulerian solver	51st AIAA/SAE/ASEE Joint propulsion conference	2015
Separation shock cutoff frequency in dual bell nozzles	51st AIAA/SAE/ASEE Joint propulsion conference	2015
Assessment of a conjugate heat transfer model for rocket engine cooling channels fed with supercritical methane	51st AIAA/SAE/ASEE Joint propulsion conference	2015

ERC

PE8_1

KET

Sustainable technologies & development

Interessi di ricerca

Keywords

Liquid rocket engines

propulsion

rocket nozzle

Progetti di Ricerca

Combined RANS/DNS analysis of conjugate heat transfer in rocket cooling channels

Gruppi di ricerca - Responsabile

T(H)RUST (THermal Rocket propUlsion: a Sapienza university research Team)