1. The Effects of Various Combustion Techniques in a
Subsonic Turbine-less Engine Through
Computational Investigation and Experimental
Validation
Hakob Karaoglanian
PI: Dr. Chivey Wu
Department of Mechanical Engineering
California State University, Los Angeles
3/14/2014
5. Jet A-1 Jet A
Flash point 38 °C (100 °F)
Auto-ignition
temperature
245 °C (473 °F)
Freezing point −47 °C (−53 °F) −40 °C (−40 °F)
Open air burning
temperatures
260–315 °C (500–599 °F)
Density at 15 °C
(59 °F)
.804 kg/L
(6.71 lb/US gal)
.820 kg/L
(6.84 lb/US gal)
Specific energy 43.15 MJ/kg 43.02 MJ/kg
Energy density 34.7 MJ/L 35.3 MJ/L
Typical Physical Properties of Jet Fuel
6. • Air inlet
• Mach 2-4
• Combustor
• Nozzle
• No moving parts
• Cannot self-start
How do they work ?
Ramjet
13. Wind Tunnel Model
Development
Hacker B20-26L DC Motor
Specifications:
Operating Current 10 A
Peak Amps 57 A
Peak Watts 220 W
RPM/V 2077
Motor Diameter 20 mm
Motor Length 44.5 mm
Shaft Diameter 2.3 mm
Shaft Length 10 mm
Weight 58g (2.03 oz)
JetPro DF-70 Ducted Fan
Specifications:
Inner Diameter: 69 mm
Outer Diameter: 72 mm
Rotor: 8 Blade
Max Motor Diameter 29 mm
Motor Shaft Diameter 3.17 mm
Total Weight 54.5g (1.92 oz)
18. Objectives
• Build upon the first series Turbine-less engine
• Make more efficient
• Develop mixing chamber
• Conical
• Cylindrical
• Tangential
• Incorporate different
combustible fuels
• The Fuel used in this study is
Propane
21. New EDF Specifications
Mercury Alloy 64mm 4700KV EDF
Specifications:
Operating Current 13 A
Peak Amps 76 A
Peak Watts 1140 W
RPM/V 1857
Motor Diameter 21 mm
Motor Length 45 mm
Shaft Diameter 2.5 mm
Shaft Length 10 mm
Weight 162g
Installed Max Thrust 1600g
Number of Blades 8
25. Combustion Results
y = 0.0214x0.8664
y = 0.0234x0.8635
0.3
0.5
0.7
0.9
1.1
1.3
1.5
1.7
20 40 60 80 100 120 140
Thrust(N)
Power (W)
Thrust vs. Power
No Combustion
Combustion
Power (No Combustion)
Power (Combustion)
32. Future Work
• Create “Final Product”
• Stay with 1” Mixing Chamber
• More Power / New Fan
• Transitional Pieces
• Single Fuel Injection line
• Write my Thesis!!
33.
34. Thank You !!
• I would like to thank the following:
• Dr. Chivey Wu
• Joseph David Wells
• I would like to give special thanks to:
• Dr. Margaret Jefferson
• Dr. Katrina Yamazaki
• LSAMP
• I would to acknowledge our special guest:
• Dr. Lisa Hammersley
• The material presented is based upon work
supported by the National Science Foundation
under Grant #HDR-1246662