hypersonic fuels chemistry: n-heptane cracking and combustion andrew mandelbaum - dept. of...

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Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand - Dept. of Mechanical Engineering, University of Illinois at Chicago Prof. Kenneth Brezinsky - Dept. of Mechanical Engineering, University of Illinois at Chicago

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Page 1: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Hypersonic Fuels Chemistry:n-Heptane Cracking and Combustion

Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University

Alex Fridlyand - Dept. of Mechanical Engineering, University of Illinois at Chicago

Prof. Kenneth Brezinsky - Dept. of Mechanical Engineering, University of Illinois at Chicago

Page 2: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Outline

•Project Background•Hypothesis•Experimental Apparatus and Methods•Results and Modeling

▫Heptane Pyrolysis▫Heptane Oxidation▫Heptane/Ethylene Oxidation

•Conclusions

Page 3: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Project Background

•Heat management•Very short reaction time requirements

Fig. 1: Cross-sectional diagram of a scramjet engine1

1. How Scramjets Work [online]. NASA. 2 Sept. 2006. 4 June 2011. http://www.nasa.gov/centers/langley/news/factsheets/X43A_2006_5.html.

Page 4: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Project Background

•Use fuel to cool engine structure

•Shorter cracking products may ignite more readily

Fig. 2: Ignition delay vs. temperature for various pure

gases and mixtures2

2. M. Colket, III and L. Spadaccini: Journal of Propulsion and Power, 2001, 17.2, 319.

Page 5: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Consequence, Questions Raised, Applications

•Injected fuel – different from fuel in tank•Effect on combustion products?•What causes the change in energy output –

physical or chemical differences?•Improved chemical simulations

▫Improved accuracy▫Use in engine modeling software▫Possibility for fuel composition customization

Page 6: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Hypothesis

•Heptane cracking products (primarily ethylene) will chemically influence combustion of remaining fuel

•Resultant species - differ in from non-cracked fuel alone and from existing heptane models

Page 7: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Low Pressure Shock Tube

•Designed to operate from 0.1-10 bar, 800-3000 K, 1-3 ms reaction time

•Explore oxidation chemistry at pressures relevant to hypersonic engine combustor

Fig. 3: Schematic drawing of low pressure shock tube and related assemblies

Page 8: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Methods• Perform pyrolysis and oxidation shocks at 4 bar

driver pressure• Examine stable intermediates and fuel decay

process using gas chromatography (GC-FID/TCD)

• Model used: n-Heptane Mechanism v3, Westbrook et al3, 4, 5

• Note: all graphs have x-error of ±5-10 K (from pressure transducers) and y-error of ±5-10% (from standards used in calibrations and GC error). Error bars are omitted for clarity

3. Mehl, M., H.J. Curran, W.J. Pitz and C.K. Westbrook: "Chemical kinetic modeling of component mixtures relevant to gasoline," European Combustion Meeting, 2009. 4. Mehl, M., W.J. Pitz, M. Sjöberg and J.E. Dec: “Detailed kinetic modeling of low-temperature heat release for PRF fuels in an HCCI engine,” S AE 2009 International Powertrains, Fuels and Lubricants Meeting, SAE Paper No. 2009-01-1806, Florence, Italy, 2009. 5. Curran, H. J., P. Gaffuri, W. J. Pitz, and C. K. Westbrook: Combustion and Flame,1998, 114, 149-177

Page 9: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane Pyrolysis

• Pyrolyze to characterize decomposition and species formed

900 950 1000 1050 1100 1150 1200 1250 1300 1350 1400 14500

10

20

30

40

50

60

T5 Calibrated [K]

He

pta

ne

Co

nce

ntr

atio

n [p

pm

]

Heptane Decomposition - Pyrolysis

Fig. 4: Concentration of heptane vs. T5 during pyrolysis

Pdriver=4 barRxn time: 1.5-1.8 ms

Page 10: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane Pyrolysis (Continued)

• Ethylene is the primary product by concentration

900 950 1000 1050 1100 1150 1200 1250 1300 1350 1400 14500

20

40

60

80

100

120

140

T5 Calibrated [K]

Eth

yle

ne

Co

nce

ntr

atio

n [p

pm

]

Ethylene Concentration - Pyrolysis

Fig. 5: Concentration of ethylene vs. T5 during pyrolysis

Pdriver=4 barRxn time: 1.5-1.8 ms

Page 11: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane Pyrolysis (Continued)

•Possible directions for future research

Fig. 6: Concentration of acetylene, methane, and propylene vs. T5 during pyrolysis

900 950 1000 1050 1100 1150 1200 1250 1300 1350 1400 14500

10

20

30

40

50

60

70

T5 Calibrated [K]

Co

nce

ntr

atio

n [p

pm

]

Acetylene, Methane, and Propylene Concentration

Acetylene

MethanePropylene

Page 12: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane Pyrolysis - Modeling

•Model results to validate shock tube operation

950 1000 1050 1100 1150 1200 1250 1300 1350 1400-10

0

10

20

30

40

50

60

T5 [K]

Co

nce

ntr

atio

n [p

pm

]

Heptane Concentration vs. Final Temperature

Heptane Pyrolysis (Data)

Heptane Pyrolysis (Model)

Fig. 7: Comparison of pyrolysis data to model results for heptane decomposition

Pdriver=4 barRxn time: 1.5-1.8 ms

Page 13: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane Oxidation – Modeling and Data

Fig. 8: Comparison of oxidation data to model results for oxygen concentration

900 950 1000 1050 1100 1150 1200 1250 1300 1350 14000

50

100

150

200

250

300

350

400

450

T5 [K]

Co

nce

ntr

atio

n [p

pm

]

Oxygen Concentration vs. Final Temperature

O2 Concentration (Data)

O2 Concentration (Model)

Pdriver=4 barRxn time: 1.5-1.8 msΦ=1.38

Page 14: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane Oxidation – Modeling and Data (Cont’d)

Fig. 9: Comparison of oxidation data to model results for ethylene concentration

Pdriver=4 barRxn time: 1.5-1.8 msΦ=1.38

900 950 1000 1050 1100 1150 1200 1250 1300 1350 1400 14500

20

40

60

80

100

120

T5 [K]

Co

nce

ntr

atio

n [p

pm

]Ethylene Concentration vs. Final Temperature

Ethylene Production (Data)

Ethylene Production (Model)

Page 15: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane Oxidation – Modeling and Data (Cont’d)

Fig. 10: Comparison of oxidation data to model results for carbon monoxide production

900 950 1000 1050 1100 1150 1200 1250 1300 1350 1400-50

0

50

100

150

200

250

T5 [K]

Co

nce

ntr

atio

n [p

pm

]Carbon Monoxide Concentration vs. Final Temperature

CO Production (Data)

CO Production (Model)

Pdriver=4 barRxn time: 1.5-1.8 msΦ=1.38

Page 16: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane with Ethylene Oxidation

Fig. 11: Normalized heptane concentration and ethylene concentration vs. T5 for neat mixture and cracked fuel mixture

900 950 1000 1050 1100 1150 1200 1250 1300 1350 1400 14500

0.2

0.4

0.6

0.8

1

T5 Calibrated [K]

He

pta

ne

Co

nce

ntr

atio

n [p

pm

]

Normalized Heptane Decomposition - Neat vs. Cracked Mixture

Cracked Fuel Mix

Neat Heptane

900 950 1000 1050 1100 1150 1200 1250 1300 1350 1400 14500

0.5

1

1.5

2

2.5

T5 Calibrated [K]

Eth

yle

ne

Co

nce

ntr

atio

n [p

pm

]

Normalized Ethylene Concentration - Neat vs. Cracked Micture

Neat Heptane (Data)

Cracked Fuel Mix (Data)

Neat Heptane (Model)

Cracked Fuel Mix (Model)

Page 17: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane with Ethylene Oxidation

Figure 12: Carbon monoxide concentration vs. T5 for pure heptane oxidation and heptane with ethylene

900 950 1000 1050 1100 1150 1200 1250 1300 1350 1400-50

0

50

100

150

200

250

300

T5 Calibrated [K]

Ca

rbo

n M

on

oxi

de

Co

nce

ntr

atio

n [p

pm

]Carbon Monoxide Concentration - Neat vs. Cracked Micture

Neat Heptane (Data)

Cracked Fuel Mix (Data)

Neat Heptane (Model)

Cracked Fuel Mix (Model)

Pdriver=4 barRxn time: 1.5-1.8 msΦ=1.38

Page 18: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Conclusions and Future Work

•Heptane cracking products affect combustion of non-cracked fuel through chemical processes

•CO, CO2, and H2O production - energy output differences

•Future experiments - other cracking products and/or different reaction pressures

Page 19: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Acknowledgements•National Science Foundation, EEC-NSF

Grant # 1062943•University of Illinois at Chicago REU•Prof. Christos Takoudis and Dr. Gregory

Jursich•Arman Butt and Runshen Xu

Page 20: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Questions

6. http://www.af.mil/shared/media/photodb/photos/100520-F-9999B-111.jpg

6

Page 21: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Calibrations

• Temperature calibrations using TFE and CPCN• Known decomposition rates allow these species to be

used as chemical thermometers

Fig. 13: TFE and CPCN shock calibration results

575 625 675 725 775 825 875850

950

1050

1150

1250

1350

1450

1550

TFE and CPCN Calibrations for 1, 4, and 10 bar

W [m/s]

T5

[K]

Page 22: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane with Ethylene Oxidation (Cont’d)

Fig. 14: Butene concentration vs. T5 for neat mixture and cracked fuel mixture

900 950 1000 1050 1100 1150 1200 1250 1300 1350 1400 14500

1

2

3

4

5

6

7

8

9

10

T5 Calibrated [K]

Bu

ten

e C

on

cen

tra

tion

[pp

m]

Butene Concentration - Neat vs. Cracked Micture

Cracked Fuel Mix

Neat Heptane

Page 23: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane with Ethylene Oxidation (Cont’d)

900 950 1000 1050 1100 1150 1200 1250 1300 1350 1400 14500

50

100

150

200

250

300

350

400

450

T5 Calibrated [K]

Oxy

gen

Con

cent

ratio

n [p

pm]

Oxygen Concentration - Neat vs. Cracked Micture

Cracked Fuel Mix

Neat Heptane

Fig. 15: Oxygen concentration vs. T5 for neat mixture and cracked fuel mixture

Page 24: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane w/ Ethylene - Modeling

•Model cracked fuel mix with and without complete hydrogen balance to validate mixture

800 1000 1200 1400 1600 1800 2000-50

0

50

100

150

200

250

300

Temperature T5 [K]

CO

Con

cent

ratio

n [p

pm]

CO Concentration vs. Final Temperature

Neat CO Production

CO Production w/ H2 Balance

CO Production w/o H2 Balance

Fig. 16: Carbon monoxide concentration vs. T5 for neat mixture and mixtures with and without hydrogen balance

Page 25: Hypersonic Fuels Chemistry: n-Heptane Cracking and Combustion Andrew Mandelbaum - Dept. of Mechanical Engineering, Princeton University Alex Fridlyand

Heptane w/ Ethylene – Modeling (Cont’d)

•Decreased H2O output without H balance

800 1000 1200 1400 1600 1800 2000-50

0

50

100

150

200

250

300

350

Temperature T5 [K]

H2O

Con

cent

ratio

n [p

pm]

H2O Concentration vs. Final Temperature

Neat H2O Production

H2O Production w/ H2 Balance

H2O Production w/o H2 Balance

Fig. 17: Water concentration vs. T5 for neat mixture and mixtures with and without hydrogen balance