Academic literature on the topic 'Aeronautic emissions'
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Journal articles on the topic "Aeronautic emissions":
Talero, Gabriel, Camilo Bayona-Roa, Giovanny Muñoz, Miguel Galindo, Vladimir Silva, Juan Pava, and Mauricio Lopez. "Experimental Methodology and Facility for the J69-Engine Performance and Emissions Evaluation Using Jet A1 and Biodiesel Blends." Energies 12, no. 23 (November 28, 2019): 4530. http://dx.doi.org/10.3390/en12234530.
Riba, Jordi-Roger, Álvaro Gómez-Pau, Manuel Moreno-Eguilaz, and Santiago Bogarra. "Arc Tracking Control in Insulation Systems for Aeronautic Applications: Challenges, Opportunities, and Research Needs." Sensors 20, no. 6 (March 16, 2020): 1654. http://dx.doi.org/10.3390/s20061654.
Frosina, Emma, Adolfo Senatore, Luka Palumbo, Giuseppe Di Lorenzo, and Ciro Pascarella. "Development of a Lumped Parameter Model for an Aeronautic Hybrid Electric Propulsion System." Aerospace 5, no. 4 (October 4, 2018): 105. http://dx.doi.org/10.3390/aerospace5040105.
Palma, Giorgio, and Lorenzo Burghignoli. "On the integration of acoustic phase-gradient metasurfaces in aeronautics." International Journal of Aeroacoustics 19, no. 6-8 (September 10, 2020): 294–309. http://dx.doi.org/10.1177/1475472x20954404.
Palma, Giorgio, Lorenzo Burghignoli, Francesco Centracchio, and Umberto Iemma. "Innovative Acoustic Treatments of Nacelle Intakes Based on Optimised Metamaterials." Aerospace 8, no. 10 (October 14, 2021): 296. http://dx.doi.org/10.3390/aerospace8100296.
Talero, Gabriel, Camilo Bayona-Roa, Vladimir Silva, Manuel Mayorga, Juan Pava, and Mauricio Lopez. "Biodiesel substitution in a J69 aeronautic turbine engine: An experimental assessment of the effects on energy efficiency, technical performance and emissions." Sustainable Energy Technologies and Assessments 40 (August 2020): 100746. http://dx.doi.org/10.1016/j.seta.2020.100746.
Zaccaria, Valentina, Amare D. Fentaye, Mikael Stenfelt, and Konstantinos G. Kyprianidis. "Probabilistic Model for Aero-Engines Fleet Condition Monitoring." Aerospace 7, no. 6 (May 26, 2020): 66. http://dx.doi.org/10.3390/aerospace7060066.
Amoroso, Francesco, Angelo De Fenza, Giuseppe Petrone, and Rosario Pecora. "A Sensitivity Analysis on the Influence of the External Constraints on the Dynamic Behaviour of a Low Pollutant Emissions Aircraft Combustor-Rig." Archive of Mechanical Engineering 63, no. 3 (September 1, 2016): 435–54. http://dx.doi.org/10.1515/meceng-2016-0025.
Hashmi, Nauman Ehsan, and Atif Manzoor. "International Aeronautical Emission." International Journal of Aviation Technology, Engineering and Management 1, no. 1 (January 2011): 30–36. http://dx.doi.org/10.4018/ijatem.2011010103.
Langat, Rogers K., Emmanuel De Luycker, Arthur Cantarel, and Micky Rakotondrabe. "Integration Technology with Thin Films Co-Fabricated in Laminated Composite Structures for Defect Detection and Damage Monitoring." Micromachines 15, no. 2 (February 15, 2024): 274. http://dx.doi.org/10.3390/mi15020274.
Dissertations / Theses on the topic "Aeronautic emissions":
Eastham, Sebastian D. (Sebastian David). "Human health impacts of high altitude emissions." Thesis, Massachusetts Institute of Technology, 2015. http://hdl.handle.net/1721.1/98585.
This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.
Cataloged from student-submitted PDF version of thesis.
Includes bibliographical references (pages 132-159).
Millions of deaths worldwide are attributed annually to exposure degraded surface air quality and UV-induced skin cancer. However, the focus has been on surface emissions, and the contribution of high altitude emissions to these issues is rarely examined. In this thesis, potential links are investigated between high altitude emissions and damages or benefits to human health via photochemical effects. Changes in population exposure to fine particulate matter, ozone and UV-B radiation resulting from current and future high altitude emissions are calculated, applying epidemiologically-derived impact functions to estimate resultant mortality and morbidity. A stratospheric extension is developed for the widely-used tropospheric model GEOS-Chem, which has been shown to accurately model tropospheric conditions and used in simulations of remote and urban pollution. This extended model, the GEOS-Chem UCX, can propagate a stratospheric perturbation through to a tropospheric impact, including shortwave UV fluxes, long-lived species, stratospheric water chemistry and high altitude aerosols. This model is employed to estimate the impacts of reversing 1 K of global warming using stratospheric sulfate aerosol injection. In total, it is projected that 85,000 additional premature mortalities would occur in 2040 due to particulate matter exposure, but that reduced ozone loading would prevent 64,000 mortalities worldwide. Aerosol injection also results in a 5.7% reduction in the global ozone column and a 3.0% increase in surface UV-B, which could cause 3,700 additional melanoma mortalities per year. By comparison, surface air quality and UV-B impacts due to aviation emissions are found to have resulted in 16,000 premature mortalities globally in 2006, of which 450 occurred in North America. Ozone exposure contributes 43% of this total. The increase in tropospheric ozone due to aviation emissions is found to have prevented 390 skin cancer mortalities in 2006. This thesis quantifies the photochemical mechanisms connecting future and proposed high altitude emissions schemes to human health impacts and provides an estimate of mortality and morbidity attributable to aviation and sulfate aerosol injection.
by Sebastian D. Eastham.
Ph. D.
Prashanth, Prakash. "Post-combustion emissions control for aero-gas turbine engines." Thesis, Massachusetts Institute of Technology, 2018. https://hdl.handle.net/1721.1/122402.
Cataloged from PDF version of thesis.
Includes bibliographical references (pages 47-50).
Aviation NO[subscript x] emissions have an impact on air quality and climate change, where the latter is magnified due to the higher sensitivity of the upper troposphere and lower stratosphere. In the aviation industry, efforts to increase the efficiency of propulsion systems are giving rise to higher overall pressure ratios which results in higher NO[subscript x] emissions due to increased combustion temperatures. This thesis identifies that the trend towards smaller engine cores (gas generators) that are power dense and contribute little to the thrust output presents new opportunities for emissions control that were previously unthinkable when the core exhaust stream contributed significant thrust. This thesis proposes and assesses selective catalytic reduction (SCR), which is a post-combustion emissions control method used in ground-based sources such as power generation and heavy-duty diesel engines, for use in aero-gas turbines.
The SCR system increases aircraft weight and introduces a pressure drop in the core stream. The effects of these are evaluated using representative engine cycle models provided by a major aero-gas turbine manufacturer. This thesis finds that employing an ammonia-based SCR can achieve close to 95% reduction in NO[subscript x] emissions for ~0.4% increase in block fuel burn. The large size of the catalyst needs to be housed in the body of the aircraft and hence would be suitable for future designs where the engine core is also within the fuselage, such as would be possible with turbo-electric or hybrid-electric designs. The performance of the post-combustion emissions control is shown to improve for smaller core engines in new aircraft in the NASA N+3 time-line (2030-2035), suggesting the potential to further decrease the cost of the ~95% NO[subscript x] reduction to below ~0.4% fuel burn.
Using a global chemistry and transport model (GEOS-Chem) this thesis estimates that using ultra-low sulfur (<15 ppm fuel sulfur content) in tandem with post-combustion emissions control results in a ~92% reduction in annual average population exposure to PM₂.₅ and a ~95% reduction in population exposure to ozone. This averts approximately 93% of the air pollution impact of aviation.
by Prakash Prashanth.
S.M.
S.M. Massachusetts Institute of Technology, Department of Aeronautics and Astronautics
Allaire, Douglas L. "A physics-based emissions model for aircraft gas turbine combustors." Thesis, Massachusetts Institute of Technology, 2006. http://hdl.handle.net/1721.1/35584.
Includes bibliographical references (p. 103-105).
In this thesis, a physics-based model of an aircraft gas turbine combustor is developed for predicting NO. and CO emissions. The objective of the model is to predict the emissions of current and potential future gas turbine engines within quantified uncertainty bounds for the purpose of assessing design tradeoffs and interdependencies in a policy-making setting. The approach taken is to capture the physical relationships among operating conditions, combustor design parameters, and pollutant emissions. The model is developed using only high-level combustor design parameters and ideal reactors. The predictive capability of the model is assessed by comparing model estimates of NO, and CO emissions from five different industry combustors to certification data. The model developed in this work correctly captures the physical relationships between engine operating conditions, combustor design parameters, and NO. and CO emissions. The NO. estimates are as good as, or better than, the NO. estimates from an established empirical model; and the CO estimates are within the uncertainty in the certification data at most of the important low power operating conditions.
by Douglas L. Allaire.
S.M.
Jun, Mina. "Microphysical modeling of ultrane hydrocarbon-containing aerosols in aircraft emissions." Thesis, Massachusetts Institute of Technology, 2011. http://hdl.handle.net/1721.1/67064.
This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.
Cataloged from student submitted PDF version of thesis.
Includes bibliographical references (p. 109-115).
Combustion engines emit precursors of ne particulate matter (PM) into the atmosphere. Numerous gaseous species, soot particles, and liquid aerosols in the aircraft exhaust are involved in PM formation, and these very ne, nanometer-size particles potentially have signicant impacts on climate, human health, and air quality. In particular, the organic content of the particles is important to determine physical and chemical properties of PM and consequently their potential impacts on the environment. The main objective of this thesis is to understand the role of organic compounds in PM evolution by developing a microphysical model that incorporates organic compounds into the formation mechanism of binary aqueous aerosols. While binary aerosol models with sulfuric acid and water have been widely studied, the understanding of the effect of organics on the formation and growth of aerosols is still insufficient. This work demonstrates important interactions and competitions in the formation of multi-component aerosols with organic compounds, sulfuric acid, and water in aircraft emissions. Hydrocarbon-containing aerosols have been identied as a major component of ground-level aircraft emission, especially at low power operations. This thesis describes selected surrogates of organic species and introduces estimation techniques for their thermophysical properties. The surrogates of organic species include water-insoluble hydrocarbons and water-soluble oxygenated hydrocarbons. Simulation results suggest that certain hydrocarbon compounds play an important role in the formation of aviation aerosol with interactions with both homogeneous sulfuric acidwater aerosols and soot particles in the organic-rich aircraft plume. Hydrocarbons contribute to the growth of existing homogeneous liquid particles, whereas their contribution to aerosol number density is negligible compared to that of sulfuric acid and water, which largely determine the formation of homogeneous aerosols. Also, low volatility hydrocarbons (e.g., benzopyrene, coronene) are observed to be partitioned into soot particles and induce competition with the uptake of water-soluble species, while light water-soluble oxygenated hydrocarbons enhance the uptake of water and sulfuric acid on soot particles.
by Mina Jun.
Ph.D.
Dorbian, Christopher S. (Christopher Salvatore). "Estimating the environmental benefits of aviation fuel and emissions reductions." Thesis, Massachusetts Institute of Technology, 2010. http://hdl.handle.net/1721.1/59668.
Cataloged from PDF version of thesis.
Includes bibliographical references (p. 99-103).
With commercial aviation continuing to grow and environmental policymaking activity intensifying, it is becoming increasingly necessary to assess the environmental impact of measures that result in changes in aviation fuel bum levels. For estimating air quality and climate impacts, it is important to employ a multi-gas approach that accounts for the effects of all emitted species, not just carbon dioxide (CO₂). The main objective of this thesis is to develop a simplified framework for monetizing the CO₂ and non-CO₂ co-benefits of aviation fuel and emissions reductions. The approach is based on two main pieces, both of which are derived using the Aviation environmental Portfolio Management Tool (APMT). First, the air quality marginal damage cost of a unit of fuel is estimated using an air quality response surface model. Second, a simplified probabilistic impulse response function model for climate is employed to derive a non-CO₂/CO₂ impact ratio that can be multiplied by a social cost of carbon to estimate the additional benefits of fuel bum reductions from aviation beyond those associated with CO2 alone. The sensitivity of the non-CO₂/CO₂ climate ratio to metric choice, scientific assumptions, background scenarios, and other policymaker choices is explored. Notably, it is found that given the large uncertainties in short-lived effects, the choice of metric is not particularly influential on the overall ratio value (that is, similar results-within the range of uncertainty-are found for the different metrics considered). This thesis also validates the use of the climate ratios and air quality marginal damages through two sample applications. The first study explores the impact of various aviation growth scenarios and demonstrates the applicability of this framework to a multi-year analysis. The second study concerns the introduction of an advanced aircraft concept into the present-day aviation fleet and demonstrates the ability of the climate ratios to capture scientific and valuation-based uncertainties. In both cases, the derived ratios and air quality damage costs are found to be a good surrogate for a full impact analysis in APMT, relative to the overall uncertainty in estimating impacts.
by Christopher S. Dorbian.
S.M.
Lee, Joosung Joseph 1974. "Historical and future trends in aircraft performance, cost, and emissions." Thesis, Massachusetts Institute of Technology, 2000. http://hdl.handle.net/1721.1/8825.
Includes bibliographical references (p. 141-144).
Air travel is continuing to experience the fastest growth among all modes of transport. Increasing total fuel consumption and the potential impacts of aircraft engine emissions on the global atmosphere have motivated the industry, scientific community, and international governments to seek various emissions reduction options. Despite the efforts to understand and mitigate the impacts of aviation emissions, it still remains uncertain whether proposed emissions reduction options are technologically and financially feasible. This thesis is the first of its kind to analyze the relationship between aircraft performance and cost, and assess aviation emissions reduction potential based on analytical and statistical models founded on a database of historical data. Technological and operational influences on aircraft fuel efficiency were first quantified utilizing the Breguet range equation. An aviation system efficiency parameter was defined, which accounts for fuel efficiency and load factor. This parameter was then correlated with direct operating cost through multivariable statistical analysis. Finally, the influence of direct operating cost on aircraft price was statistically determined. By comparing extrapolations of historical trends in aircraft technology and operations with future projections in the open literature, the fuel burn reduction potential for future aircraft systems was estimated. The economic characteristics of future aircraft systems were then determined by utilizing the technology-cost relationship developed in the thesis. Although overall system efficiency is expected to improve at a rate of 1.7% per year, it is not sufficient to counter the projected annual 4 to 6% growth in demand for air transport. Therefore, the impacts of aviation emissions on the global atmosphere are expected to continue to grow. Various policy options for aviation emissions reduction and their potential effectiveness are also discussed.
by Joosung Loseph Lee.
S.M.
Lee, Joosung Joseph 1974. "Modeling aviation's global emissions, uncertainty analysis, and applications to policy." Thesis, Massachusetts Institute of Technology, 2005. http://hdl.handle.net/1721.1/28917.
Includes bibliographical references (p. 131-134).
(cont.) fuel burn results below 3000 ft. For emissions, the emissions indices were the most influential uncertainties for the variance in model outputs. By employing the model, this thesis examined three policy options for mitigating aviation emissions. More stringent engine certification standards, continuous descent approach procedures, and derated take-off procedures were analyzed. Uncertainties of the model were carefully accounted for in the fuel burn and emissions scenarios of the policy options. The considered policy options achieved roughly 10-30% reductions in NOx emissions. However, HC and CO emissions rather increased due to higher emissions production rate for the CDA and derated take-off. In addition, the NOx emissions reductions in some cases were not statistically significant given the uncertainty in the modeling tool.
Air travel continues to experience fast growth. Although the energy intensity of the air transport system continues to improve, aviation fuel use and emissions of many pollutants have risen. This thesis focuses on developing, assessing and applying a system model to evaluate global aircraft fuel consumption and emissions, and to examine technological and operational measures to mitigate these emissions. The model is capable of computing how much emissions are produced on a flight-by-flight, fleet and global basis and where in the atmosphere the emissions are deposited. These are important questions for aviation environmental policy-making. Model development was followed by a comprehensive uncertainty analysis. It involved comparisons of reported versus modeled results at both the modular and system levels. On average, the aggregate-level composite fuel burn results showed about -6% difference from reported fuel burn data. A statistical analysis showed that this mean shift was a combined contribution of the key uncertainties in aircraft performance and operations. A parametric study followed to rank-order the effects that the key modeling uncertainties had on estimates of fuel burn and emissions. Statistical methods were developed to analyze both the random and systematic errors of the modeling tools. The analyses showed that the uncertainties in engine and aerodynamic performance had the largest impact on system errors, accounting for around 60-70% of the total variance in full-mission fuel burn results. The uncertainties in winds aloft and take-off weight explained another 20-25%. LTO procedures, which consist of engine throttle setting, rate of climb/descent and flight speed, were the most influential uncertainties that drove the variance in
by Joosung Joseph Lee.
Ph.D.
Dedoussi, Irene Constantina. "Adjoint sensitivity analysis of the atmospheric impacts of combustion emissions." Thesis, Massachusetts Institute of Technology, 2018. http://hdl.handle.net/1721.1/120414.
Cataloged from PDF version of thesis.
Includes bibliographical references (pages 127-149).
Combustion emissions impact the environment through chemical and transport processes that span varying temporal and spatial scales. Numerical simulation of the effects of combustion emissions and potential corresponding mitigation approaches is computationally expensive. Atmospheric adjoint modeling enables the calculation of receptor-oriented sensitivities of environmental metrics of interest to emissions, overcoming the numerical cost of conventional modeling. This thesis applies and further develops an existing adjoint of a chemistry-transport model to perform three evaluations, where the high number of inputs (due to the nature of the problem or the associated uncertainty) prevented comprehensive assessment in the past. First, this thesis quantifies the pollution exchange between the US states for seven major anthropogenic combustion emissions sectors: electric power generation, industry, commercial/residential, aviation, as well as road, marine, and rail transportation. This thesis presents the state-level fine particulate matter (PM₂.₅) early death impacts of combustion emissions in the US for 2005, 2011 and 2018 (forecast), and how these are driven by sector, chemical species, and location of emission. Results indicate major shifts in the chemical species and sectors that cause most early deaths, and opportunities for further improving air quality in the US. Second, this thesis quantifies how changes in emissions impact the marginal atmospheric PM₂.₅ response to emissions perturbations. State-level annual adjoint sensitivities of PM₂.₅ population exposure to precursor emissions are compared for the years of 2006 and 2011, and correlated with the magnitude of emissions reduction and the background ammonia mixing ratio. Third, this thesis presents the development and evaluation of the discrete adjoint of the GEOS-Chem unified tropospheric-stratospheric chemistry extension (UCX), which enables the calculation of stratospheric sensitivities and the examination of the entire design space of high altitude emissions impacts. To illustrate its potential, sensitivities of stratospheric ozone to precursor species are calculated. This development expands the span of atmospheric chemistry-transport questions (including inversions) that this open-source model can be used to answer. The assessments performed in this thesis span spatial scales from the regional to the global and demonstrate the ability of this approach to provide information on both bottom-up and top-down mitigation approaches.
by Irene Constantina Dedoussi.
Ph. D.
Galligan, Timothy R. "CO₂ emissions reduction potential of aviation biofuels in the US." Thesis, Massachusetts Institute of Technology, 2018. https://hdl.handle.net/1721.1/122397.
Cataloged from PDF version of thesis.
Includes bibliographical references (pages 55-60).
Aviation biofuels derived from biomass and wastes have been identified as a means to reduce carbon dioxide (CO₂) emissions from US aviation, but the magnitude of the possible reduction has not been quantified. This scenario-based analysis quantifies the life cycle greenhouse gas (GHG) mitigation potential of aviation biofuels in 2050 within the US. Projected arable land availability, growth in agricultural yields, and the availability of wastes and residues are estimated as a function of future economic and climate patterns, and variability is accounted for. Under a baseline set of assumptions, the use of aviation biofuels results in a maximum reduction of 163 Tg of CO₂ equivalent (CO₂e) in 2050, a 42% reduction in life cycle GHG emissions compared to petroleum-derived jet fuel. Across all scenarios assessed, the reduction in life cycle GHGs ranges from 47.0 to 207 Tg CO₂e (12-53%), requiring the use of fuels derived from wastes, agriculture and forestry residues, and cultivated energy crops. Using only fuels derived from residues and wastes, up to 35% of US jet fuel demand could be met, corresponding to a 28% reduction of CO₂e. The results are most sensitive to assumptions on the distribution of fuel products, and agricultural residue availability.
by Timothy R. Galligan.
S.M.
S.M. Massachusetts Institute of Technology, Department of Aeronautics and Astronautics
Gill, Simaranjit Singh. "Controlling diesel NO_x & PM emissions using fuel components and enhanced aftertreatment techniques : developing the next generation emission control system." Thesis, University of Birmingham, 2012. http://etheses.bham.ac.uk//id/eprint/3643/.
Books on the topic "Aeronautic emissions":
Great Britain. Dept. for Transport., ed. UK air passenger demand and CO₂ forecasts. London: Dept. for Transport, 2009.
1968-, Klingmüller Angela, Steppler Ulrich 1970-, European Parliament, European Parliament, and European Parliament, eds. EU emissions trading scheme and aviation. Utrecht: Eleven International Publishing, 2010.
Geisler, Markus, Stephan Hobe, and Marius Boewe. Luftverkehr und Klimawandel. Berlin: Lit, 2009.
United States. Congress. House. Committee on Transportation and Infrastructure. Subcommittee on Aviation. The European Union's emissions trading scheme: A violation of international law : hearing before the Subcommittee on Aviation of the Committee on Transportation and Infrastructure, House of Representatives, One Hundred Twelfth Congress, first session, July 27, 2011. Washington: U.S. G.P.O., 2012.
National Research Council (U.S.). Committee on Aeronautics Research and Technology for Environmental Compatibility. For greener skies: Reducing environmental impacts of aviation. Washington, D.C: National Academy Press, 2002.
JANNAF Exhaust Plume Technology Subcommittee. Meeting. 21st JANNAF Exhaust Plume Technology Subcommittee meeting: Lockheed Missiles and Space Company, Sunnyvale, CA, 19-21 October 1994. Edited by Gannaway Mary T, Johns Hopkins University. Chemical Propulsion Information Agency., and Lockheed Missiles and Space Company. Columbia, MD: Johns Hopkins University, Chemical Propulsion Information Agency, 1994.
United States. National Aeronautics and Space Administration., ed. Implementation of ADI-schemes on MIMD parallel computers. San Jose, Calif: MCAT Institute, 1993.
United States. National Aeronautics and Space Administration., ed. Implementation of ADI-schemes on MIMD parallel computers. San Jose, Calif: MCAT Institute, 1993.
United States. National Aeronautics and Space Administration., ed. Implementation of ADI-schemes on MIMD parallel computers. San Jose, Calif: MCAT Institute, 1993.
Organization, International Civil Aviation. ICAO environmental report 2007. Montreal: International Civil Aviation Organization, 2007.
Book chapters on the topic "Aeronautic emissions":
Aggelis, Dimitrios G., Markus G. R. Sause, Pawel Packo, Rhys Pullin, Steve Grigg, Tomaž Kek, and Yu-Kun Lai. "Acoustic Emission." In Structural Health Monitoring Damage Detection Systems for Aerospace, 175–217. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-72192-3_7.
Schlag, Mareike, Kai Brune, Hauke Brüning, Michael Noeske, Célian Cherrier, Tobias Hanning, Julius Drosten, et al. "Extended Non-destructive Testing for Surface Quality Assessment." In Adhesive Bonding of Aircraft Composite Structures, 119–222. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-319-92810-4_3.
Renane, Rachid, Rachid Allouche, and Nour Abdelkader. "Effects of Preheating Temperature and Fuel-Air Equivalence Ratio on Pollution Control in Hydro Carbon Combustion." In Mechanical Engineering Technologies and Applications: Volume 2, 84–104. BENTHAM SCIENCE PUBLISHERS, 2023. http://dx.doi.org/10.2174/9789815124125123020008.
Rodi*, Michael, and Michael Mehling**. "II.Energy." In European Environmental Law, 340–63. Oxford University PressOxford, 2023. http://dx.doi.org/10.1093/oso/9780199545261.003.0010.
Corcau, Jenica-Ileana, Liviu Dinca, and Ciprian-Marius Larco. "Modeling and Simulation of APU Based on PEMFC for More Electric Aircraft." In Aeronautics - New Advances [Working Title]. IntechOpen, 2022. http://dx.doi.org/10.5772/intechopen.105597.
Vieira, Carolina Correia, and Rui Castro e Quadros. "Global Commercial Aviation Zero Emissions Target." In Advances in Logistics, Operations, and Management Science, 128–49. IGI Global, 2024. http://dx.doi.org/10.4018/979-8-3693-0908-7.ch008.
Deng, Jie, and Nansha Gao. "Periodic Acoustic Black Holes to Mitigate Sound Radiation from Cylindrical Structures." In Acoustic Emission - New Perspectives and Applications. IntechOpen, 2022. http://dx.doi.org/10.5772/intechopen.101959.
Baklezos, Anargyros T., and Christos N. Capsalis. "SpaceWire." In Recent Trends on Electromagnetic Environmental Effects for Aeronautics and Space Applications, 39–79. IGI Global, 2021. http://dx.doi.org/10.4018/978-1-7998-4879-0.ch002.
Nikolopoulos, Christos D. "Recent Advances on Measuring and Modeling ELF-Radiated Emissions for Space Applications." In Recent Trends on Electromagnetic Environmental Effects for Aeronautics and Space Applications, 1–38. IGI Global, 2021. http://dx.doi.org/10.4018/978-1-7998-4879-0.ch001.
Jeevan Danaraj, Edgar. "Electrification for Aero-Engines: A Case Study of Modularization in New Product Development." In Advances in Turbomachinery [Working Title]. IntechOpen, 2022. http://dx.doi.org/10.5772/intechopen.109006.
Conference papers on the topic "Aeronautic emissions":
Trancossi, Michele. "Design of a Cogeneration Hybrid Propulsion System for Commuter Aircrafts With Thermal Recovery." In ASME 2015 9th International Conference on Energy Sustainability collocated with the ASME 2015 Power Conference, the ASME 2015 13th International Conference on Fuel Cell Science, Engineering and Technology, and the ASME 2015 Nuclear Forum. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/es2015-49815.
Bulzan, Dan, Bruce Anderson, Changlie Wey, Robert Howard, Edward Winstead, Andreas Beyersdorf, Edwin Corporan, et al. "Gaseous and Particulate Emissions Results of the NASA Alternative Aviation Fuel Experiment (AAFEX)." In ASME Turbo Expo 2010: Power for Land, Sea, and Air. ASMEDC, 2010. http://dx.doi.org/10.1115/gt2010-23524.
Ruan, Jiangheng L., Axel Vincent-Randonnier, Guillaume Pilla, and Cornelia Irimiea. "Development of Innovative Low NOx Hydrogen-Fueled Burner for Aeronautic Applications." In ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/gt2023-100453.
Duchaine, Patrick, Quentin Bouyssou, Stéphane Pascaud, Gorka Exilard, and Christophe Viguier. "Soot Emission Optimization of a Helicopter Engine: From Injector Design to Engine Tests Validation." In ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/gt2020-16100.
Kritikos, Kosmas, Emidio Giordano, Anestis I. Kalfas, and Nicolas Tantot. "Prediction of Certification Noise Levels Generated by Contra-Rotating Open Rotor Engines." In ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/gt2012-69232.
Leparoux, Julien, Renaud Lecourt, and Olivier Penanhoat. "Effect of Aromatics in Jet Fuels on Spray Characteristics Downstream of an Aeronautical Pressure Swirl Atomizer." In ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/gt2016-56565.
Caggese, S. "A parametric model for thermal management system for more electric and hybrid aircraft." In Aeronautics and Astronautics. Materials Research Forum LLC, 2023. http://dx.doi.org/10.21741/9781644902813-17.
Tong, Michael T. "A Probabilistic Risk-Based Approach to Assess NASA Aeronautics Technologies." In ASME Turbo Expo 2006: Power for Land, Sea, and Air. ASMEDC, 2006. http://dx.doi.org/10.1115/gt2006-91007.
Reddy, Dhanireddy R., and Chi-Ming Lee. "An Overview of Low-Emission Combustion Research at NASA Glenn." In ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/gt2016-56100.
Richiardi, G. "Low-boom supersonic business jet: aerodynamic analysis and mission simulation towards a CO2 emission standard." In Aeronautics and Astronautics. Materials Research Forum LLC, 2023. http://dx.doi.org/10.21741/9781644902813-27.