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1

DuBeau, Robert William. An investigation of the effects of fuel composition on combustion characteristics in a T-63 combustor. Naval Postgraduate School, 1985.

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2

K, Mongia Rajiv, Dibble Robert W, and NASA Glenn Research Center, eds. Real-time optical fuel-to-air ratio sensor for gas turbine combustors. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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3

K, Mongia Rajiv, Dibble Robert W, and NASA Glenn Research Center, eds. Real-time optical fuel-to-air ratio sensor for gas turbine combustors. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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4

K, Mongia Rajiv, Dibble Robert W, and NASA Glenn Research Center, eds. Real-time optical fuel-to-air ratio sensor for gas turbine combustors. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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5

Perkins, Hugh Douglas. Effects of fuel distribution on detonation tube performance. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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6

A, Strehlow Roger, University of Illinois at Urbana-Champaign. Aeronautical and Astronautical Engineering Dept., and United States. National Aeronautics and Space Administration., eds. The behavior of fuel-lean premixed flames in a standard flammability limit tube under controlled gravity conditions. Aeronautical and Astronautical Engineering Dept., University of Illinois, 1986.

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7

A, Strehlow Roger, University of Illinois at Urbana-Champaign. Aeronautical and Astronautical Engineering Dept, and United States. National Aeronautics and Space Administration, eds. The behavior of fuel-lean premixed flames in a standard flammability limit tube under controlled gravity conditions. Aeronautical and Astronautical Engineering Dept., University of Illinois, 1986.

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8

A, Strehlow Roger, University of Illinois at Urbana-Champaign. Aeronautical and Astronautical Engineering Dept, and United States. National Aeronautics and Space Administration, eds. The behavior of fuel-lean premixed flames in a standard flammability limit tube under controlled gravity conditions. Aeronautical and Astronautical Engineering Dept., University of Illinois, 1986.

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9

United States. National Aeronautics and Space Administration., ed. Structure of a swirl-stabilized combusting spray. American Institute of Aeronautics and Astronautics, Inc., 1995.

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10

United States. National Aeronautics and Space Administration., ed. Structure of a swirl-stabilized combusting spray. American Institute of Aeronautics and Astronautics, Inc., 1995.

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11

United States. National Aeronautics and Space Administration., ed. Structure of a swirl-stabilized combusting spray. American Institute of Aeronautics and Astronautics, Inc., 1995.

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12

United States. National Aeronautics and Space Administration., ed. Structure of a swirl-stabilized combusting spray. American Institute of Aeronautics and Astronautics, Inc., 1995.

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13

United States. National Aeronautics and Space Administration., ed. Structure of a swirl-stabilized combusting spray. National Aeronautics and Space Administration, 1994.

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14

United States. National Aeronautics and Space Administration., ed. Structure of a swirl-stabilized combusting spray. National Aeronautics and Space Administration, 1994.

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15

Han, Yongping. Spark plug based diagnostics for fuel-air ratio determination. National Library of Canada, 1998.

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16

C, Olin R., and Atmospheric Research and Exposure Assessment Laboratory (U.S.), eds. Quality assurance procedures: Project summary : method 28A, measurement of air to fuel ratio and minimum burn rate for wood-fired appliances. U.S. Environmental Protection Agency, Atmospheric Research and Exposure Assessment Laboratory, 1989.

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17

Real-time optical fuel-to-air ratio sensor for gas turbine combustors. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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18

Effects of fuel distribution on detonation tube performance. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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19

The behavior of fuel-lean premixed flames in a standard flammability limit tube under controlled gravity conditions. Aeronautical and Astronautical Engineering Dept., University of Illinois, 1986.

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20

Structure of a swirl-stabilized combusting spray. National Aeronautics and Space Administration, 1994.

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21

Structure of a swirl-stabilized combusting spray. National Aeronautics and Space Administration, 1994.

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22

Rez, Peter. Buildings. Oxford University Press, 2017. http://dx.doi.org/10.1093/oso/9780198802297.003.0003.

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Most of the energy used by buildings goes into heating and cooling. For small buildings, such as houses, heat transfer by conduction through the sides is as much as, if not greater than, the heat transfer from air exchanges with the outside. For large buildings, such as offices and factories, the greater volume-to-surface ratio means that air exchanges are more significant. Lights, people and equipment can make significant contributions. Since the energy used depends on the difference in temperature between the inside and the outside, local climate is the most important factor that determines
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23

Zoysa, Merrenna Manula De. Neural network estimation of air-fuel ratio in internal combustion engines. 2003.

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24

National Aeronautics and Space Administration (NASA) Staff. Real-Time Optical Fuel-To-Air Ratio Sensor for Gas Turbine Combustors. Independently Published, 2018.

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25

Alcott, Louisa May. Little Women: BBC Radio 4 full-cast dramatisation. BBC Audio, 2017.

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26

Conan, Doyle A. The Return of Sherlock Holmes: Twelve BBC Radio 4 Full-Cast Dramatisations. BBC Audio, 2018.

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