Department of Aerospace Engineering & Engineering ... · Jacob Gamertsfelder & Prashant Khare...

Department of Aerospace Engineering & Engineering Mechanics

Gamertsfelder & Khare/UC1

Jacob Gamertsfelder & Prashant Khare

University of Cincinnati

Injector Dynamics and Atomization Behaviors of Liquid Monopropellants in

Pintle Injectors

Acknowledgements: CEAS, University of Cincinnati, OSGC

Outline

• Background

• Current Research and Objectives

• Theoretical formulation

• Model Validation

• Operating conditions and Geometry

• Analysis

• Conclusions and future work

Background/Motivation Google images

Mark 48 Torpedo Lunar Excursion Module SpaceX Merlin Rocket Engine

Garden Hose, Monopropellant pintle injector SpaceX raptor engine bipropellant pintle injector cold flow test

Current Status and Objectives

Objectives:

• Identify the fundamental mechanisms underlying the injector dynamics and

atomization behaviors of liquid monopropellants in pintle injectors

• Quantitatively investigate the droplet size distributions and their temporal and

spatial evolution

• Conduct parametric studies to investigate these behaviors at a wide range of

Weber numbers and operating pressures

Current Status and unresolved research issues:• Limited research exists on the fundamental mechanisms underlying the

monopropellant pintle injector dynamics and atomization behaviors

• Most research is dedicated to bipropellant engines.

Multiphase & Multiscale Challenges

Weber number, We

Reynolds number, Re

Density ratio

Viscosity ratio

• Discontinuity of material properties at the interface

• Surface tension singularity force active only at the interface

• Frequent topology changes

multiphase

multiscale • Time and length scales vary over several orders of magnitude

Liquid

Governing Equations: Volume-of-Fluid Method (VOF)

• Incompressible, variable-density, Navier-Stokes equations:

• Volume fraction, two-phase fluid density and viscosity:

• Advection for volume fraction:

++−=+

nD)u)uus

0)( =+ ucct

Adaptive Mesh Refinement (AMR)

• Gradient and value based refinement

• Cells without AMR 5.49 × 1012

• Cells with AMR = 28.623 million

• Total reduction = 99.47%

• Min. cell size = 0.305µm

Adaptive Mesh Refinement (AMR)

Validation Of The Model

• Model validation will be based upon the work of Vlad Petrescu

• The model validation will be three faceted comparing

• Spray Angle

• Sauter mean diameter

• Physical inspection

Physical Properties Water (1.6psi)Chamber gas (air

atmospheric)

Density, ρ (kg/m3) 1000 1.28

Viscosity, μ (Pa∙s) 9.532x10-4 1.822x10-5

Surface Tension, σ N/m) 0.07275

Model geometry

Experimental geometry

Atomized spray properties in pintle injection , Petrescu, Schrijer and Zandbergen

Qualitative comparison with experimental measurements

20mm 40mm 55mm 70mm

From the Experiment

Liquid sheet

Ligaments

Droplet formation

Validation: SMD and spray angle comparison with experiment

Location

injector

SMD from

experiment

SMD from

present

calculations

% error

60 mm1291.32 1273.74 1.36%

65 mm 1194.56 1242.79 -4.04%

70 mm1104.14 1101.92 0.20%

60mm 70mmExperimental Present

Calculations

% error

31.0 29.7 4.2%

Otto Fuel II Chamber gas

Density, ρ (kg/m3) 1232 123.2

Viscosity, μ (Pa∙s) 0.44 2.0764 x 10-7

Surface Tension, σ N/m) 0.03445

Physical Properties and Geometry

no-slip boundary condition

3.34m/s

constant

inflow

outflow

𝜌𝑙𝑢2𝑟

𝜎We = = 500

P 10.62

T 300K

annulus

diameter, d

pintle

pintlemovement

3-D VOF

Pintle Injector Atomization at We=20

Side View

Detailed Physics: Ligament Formation 3-D

non-dimensionalized time, t = t*/(d/Uj ) = 0.0 - 0.11

Side ViewAxial view

2-D center plane slice

Detailed Physics: Ligament Formation 2-D

Tracer VOF

16 Khare/UC

non-dimensionalized time, t = t*/(d/Uj ) = 0.11- 0.21

Detailed Physics: First break-up 3-D

Axial view

Gamertsfelder & Khare/UC

3-D View

Tracer VOF

Detailed Physics: First break-up 2-D

non-dimensionalized time, t = t*/(d/Uj ) = 0.11- 0.21

2-D center plane slice

18 Khare/UC

Detailed Physics: Sheet Sheering and Break-up

non-dimensionalized time

t = t*/(d/Uj ) = 0.22 - 0.90

non-dimensionalized time

t = t*/(d/Uj ) = 0.19

3-D VOF - Outside 3-D VOF -Inside

19 Khare/UC

2-D Center Plane Slice 3-D VOF

Detailed Physics: Appearance of Kelvin-Helmholtz Instabilities

Khare/UC

center

2-D Vorticity slice

Detailed Physics: Droplet Recirculation Vortex Formation

non-dimensionalized time t = t*/(d/Uj ) = 1.24 – 1.40

21 Khare/UC

3-D VOF

non-dimensionalized time,

t = t*/(d/Uj ) = 1.64

Detailed Physics: Clumping and Droplet Coalescence Hinders Atomization

2-D Tracer Iso-line

Droplet Production Changes with Time

Khare/UC17 Gamertsfelder & Khare/UC22

Droplet Production in terms of Probability

Sauter Mean Diameter

Khare/UC21 Gamertsfelder & Khare/UC

Droplet production over time

Conclusion

• High-fidelity numerical simulations were conducted to

quantitatively identify the atomization of

monopropellant pintle injectors was investigated

• By the formation of recirculation zones slowing the

flow in the U direction.

• By the ligaments breaking inwards leading to formation

of larger droplets

• Droplet distribution analysis shows that droplet

coalescences increaces the overall sauter mean

diameter

• Droplet distribution analysis also shows an Gaussian

droplet distribution with a slowing production rate due

to droplet coalescence

Future Investigations

• Investigate and quantify the differences in breakup

and droplet distribution for different Weber numbers

and operating pressures

• Determine the effect of pintle angle and location on

droplet distribution

Questions?

Back-up

Sauter Mean diameter Comparison

20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95 100 105 110 115

Distance from the Pintle injector in mm

Extrapolated Sauter mean diameter from emperical equation

Experimental Values

Model Values

Spray Angle Comparison

Model had a 31 degree half spray angle measured at 10mm

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