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1

Kunkulagunta, K. R. Spray, combustion and emission studies in high speed DI diesel engines. Manchester: UMIST, 1995.

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2

Jankowsky, Robert S. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. [Cleveland, Ohio]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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3

Jankovsky, Robert S. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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4

Masters, Philip A. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. Cleveland, Ohio: Lewis Research Center, 1988.

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5

Kazi, Rafiq Akhtar. A high pressure kinetic study of the in-situ combustion process for oil recovery. Salford: University of Salford, 1995.

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6

Kinzler, D. D. Experimental study of high levels of SOb2 sremoval in atmospheric-pressure fluidized-bed combustors. Research Triangle Park, NC: U.S. Environmental Protection Agency, Air and Energy Engineering Research Laboratory, 1989.

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7

Kinzler, D. D. Experimental study of high levels of SO2 removal in atmospheric-pressure fluidized-bed combustors. Research Triangle Park, NC: U.S. Environmental Protection Agency, Air and Energy Engineering Research Laboratory, 1989.

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8

Kinzler, D. D. Experimental study of high levels of SO removal in atmospheric-pressure fluidized-bed combustors. Research Triangle Park, NC: U.S. Environmental Protection Agency, Air and Energy Engineering Research Laboratory, 1989.

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9

Carter, Campbell D. Saturated fluorescence measurements of the hydroxyl radical in laminar high-pressure flames. West Lafayette, Ind: Purdue University, 1990.

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10

Carter, Campbell D. Saturated fluorescence measurements of the hydroxyl radical in laminar high-pressure flames. West Lafayette, Ind: Purdue University, 1990.

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11

Kay, Charles M., and J. Karthikeyan, eds. High Pressure Cold Spray. ASM International, 2016. http://dx.doi.org/10.31399/asm.tb.hpcspa.9781627082853.

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12

Planar imaging of hydroxyl in a high temperature, high pressure combustion facility. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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13

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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14

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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15

M, Kazaroff John, Pavli Albert J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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16

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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17

High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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18

M, Kazaroff John, Pavli Albert J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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19

M, Kazaroff John, Pavli Albert J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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20

Center, NASA Glenn Research, ed. NASA GRC's high pressure burner rig facility and materials test capabilities. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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21

High pressure, earth storable rocket technology. [Washington, D.C: National Aeronautics and Space Administration], 1997.

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22

Vaillancourt, Marie Emma. High pressure soot formation in non-smoking methane-air laminar diffusion flames from 1.5 MPa to 6.0 MPa. 2006.

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23

S, Armstrong Elizabeth, Price Harold G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. [Washington, DC]: National Aeronautics and Spac14., 1988.

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24

S, Armstrong Elizabeth, Price Harold G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. [Washington, DC]: National Aeronautics and Spac14., 1988.

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25

United States. National Aeronautics and Space Administration., ed. NASA Lewis Research Center's combustor test facilities and capabilities. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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26

United States. National Aeronautics and Space Administration., ed. NASA Lewis Research Center's combustor test facilities and capabilities. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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27

United States. National Aeronautics and Space Administration., ed. Construction of a direct water-injected two-stroke engine for phased direct fuel injection-high pressure charging investigations: Order number, A49222D (LAS), April 1, 1998. Tecumseh, MI: Orbital Engine Company (USA) Inc., 1998.

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28

J, Locke Randy, and NASA Glenn Research Center, eds. Non-intrusive, laser-based imaging of Jet-A fuel injection and combustion species in high pressure, subsonic flows. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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29

J, Locke Randy, and NASA Glenn Research Center, eds. Non-intrusive, laser-based imaging of Jet-A fuel injection and combustion species in high pressure, subsonic flows. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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30

J, Locke Randy, and NASA Glenn Research Center, eds. Non-intrusive, laser-based imaging of Jet-A fuel injection and combustion species in high pressure, subsonic flows. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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31

M, Laurendeau Normand, and Lewis Research Center, eds. Laser-induced fluorescence measurements and modeling of nitric oxide in high-pressure premixed flames. Cleveland, Ohio: Lewis Research Center, National Aeronautics and Space Administration, 1994.

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32

Laser-induced fluorescence measurements and modeling of nitric oxide in high-pressure premixed flames. Cleveland, Ohio: Lewis Research Center, National Aeronautics and Space Administration, 1994.

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33

M, Laurendeau Normand, and Lewis Research Center, eds. Laser-induced fluorescence measurements and modeling of nitric oxide in high-pressure premixed flames. Cleveland, Ohio: Lewis Research Center, National Aeronautics and Space Administration, 1994.

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34

United States. National Aeronautics and Space Administration., ed. Quantitative PLIF imaging in high-pressure combustion: Final technical report for the period June 11, 1990 to September 20, 1996. Stanford, CA: High Temperature Gasdynamics Laboratory, Mechanical Engineering Department, Stanford University, 1997.

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35

Muk, Hwang Soon, Rabinowitz Martin Jay, and United States. National Aeronautics and Space Administration., eds. Shock tube and modeling study of the H + O₂ = OH + O reaction over a wide range of composition, pressure, and temperature. [Washington, DC: National Aeronautics and Space Administration, 1995.

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36

A, Knight B., Shirley J. A, and Lewis Research Center, eds. Development of UV optical measurements of nitric oxide and hydroxyl radical at the exit of high pressure gas turbine combustors: Final report (March 1995 to March 1998). [East Hartford, CT]: United Technologies Research Center, 1998.

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37

Frew, Anthony. Air pollution. Edited by Patrick Davey and David Sprigings. Oxford University Press, 2018. http://dx.doi.org/10.1093/med/9780199568741.003.0341.

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Abstract:
Any public debate about air pollution starts with the premise that air pollution cannot be good for you, so we should have less of it. However, it is much more difficult to determine how much is dangerous, and even more difficult to decide how much we are willing to pay for improvements in measured air pollution. Recent UK estimates suggest that fine particulate pollution causes about 6500 deaths per year, although it is not clear how many years of life are lost as a result. Some deaths may just be brought forward by a few days or weeks, while others may be truly premature. Globally, household pollution from cooking fuels may cause up to two million premature deaths per year in the developing world. The hazards of black smoke air pollution have been known since antiquity. The first descriptions of deaths caused by air pollution are those recorded after the eruption of Vesuvius in ad 79. In modern times, the infamous smogs of the early twentieth century in Belgium and London were clearly shown to trigger deaths in people with chronic bronchitis and heart disease. In mechanistic terms, black smoke and sulphur dioxide generated from industrial processes and domestic coal burning cause airway inflammation, exacerbation of chronic bronchitis, and consequent heart failure. Epidemiological analysis has confirmed that the deaths included both those who were likely to have died soon anyway and those who might well have survived for months or years if the pollution event had not occurred. Clean air legislation has dramatically reduced the levels of these traditional pollutants in the West, although these pollutants are still important in China, and smoke from solid cooking fuel continues to take a heavy toll amongst women in less developed parts of the world. New forms of air pollution have emerged, principally due to the increase in motor vehicle traffic since the 1950s. The combination of fine particulates and ground-level ozone causes ‘summer smogs’ which intensify over cities during summer periods of high barometric pressure. In Los Angeles and Mexico City, ozone concentrations commonly reach levels which are associated with adverse respiratory effects in normal and asthmatic subjects. Ozone directly affects the airways, causing reduced inspiratory capacity. This effect is more marked in patients with asthma and is clinically important, since epidemiological studies have found linear associations between ozone concentrations and admission rates for asthma and related respiratory diseases. Ozone induces an acute neutrophilic inflammatory response in both human and animal airways, together with release of chemokines (e.g. interleukin 8 and growth-related oncogene-alpha). Nitrogen oxides have less direct effect on human airways, but they increase the response to allergen challenge in patients with atopic asthma. Nitrogen oxide exposure also increases the risk of becoming ill after exposure to influenza. Alveolar macrophages are less able to inactivate influenza viruses and this leads to an increased probability of infection after experimental exposure to influenza. In the last two decades, major concerns have been raised about the effects of fine particulates. An association between fine particulate levels and cardiovascular and respiratory mortality and morbidity was first reported in 1993 and has since been confirmed in several other countries. Globally, about 90% of airborne particles are formed naturally, from sea spray, dust storms, volcanoes, and burning grass and forests. Human activity accounts for about 10% of aerosols (in terms of mass). This comes from transport, power stations, and various industrial processes. Diesel exhaust is the principal source of fine particulate pollution in Europe, while sea spray is the principal source in California, and agricultural activity is a major contributor in inland areas of the US. Dust storms are important sources in the Sahara, the Middle East, and parts of China. The mechanism of adverse health effects remains unclear but, unlike the case for ozone and nitrogen oxides, there is no safe threshold for the health effects of particulates. Since the 1990s, tax measures aimed at reducing greenhouse gas emissions have led to a rapid rise in the proportion of new cars with diesel engines. In the UK, this rose from 4% in 1990 to one-third of new cars in 2004 while, in France, over half of new vehicles have diesel engines. Diesel exhaust particles may increase the risk of sensitization to airborne allergens and cause airways inflammation both in vitro and in vivo. Extensive epidemiological work has confirmed that there is an association between increased exposure to environmental fine particulates and death from cardiovascular causes. Various mechanisms have been proposed: cardiac rhythm disturbance seems the most likely at present. It has also been proposed that high numbers of ultrafine particles may cause alveolar inflammation which then exacerbates preexisting cardiac and pulmonary disease. In support of this hypothesis, the metal content of ultrafine particles induces oxidative stress when alveolar macrophages are exposed to particles in vitro. While this is a plausible mechanism, in epidemiological studies it is difficult to separate the effects of ultrafine particles from those of other traffic-related pollutants.
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