Exhaust Emissions from In-Use General Aviation Aircraft (2016)

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88 Exhaust Emissions from In-Use General Aviation Aircraft Schauer, J. J., et al. 2002. “Measurement of Emissions from Air Pollution Sources. 5. C1-C32 Organic Com- pounds from Gasoline-Powered Motor Vehicles.” Environ. Sci. Technol. 36 (6):1169–1180. DOI: 10.1021/ es0108077. Timko, M. T., et al. 2010. “Gas Turbine Engine Emissions—Part I: Volatile Organic Compounds and Nitrogen Oxides.” J. Eng. Gas Turb. Power. 132 (6):061504. DOI: 10.1115/1.4000131. Timko, M. T., et al. 2010. “Gas Turbine Engine Emissions—Part II: Chemical Properties of Particulate Matter.” J. Eng. Gas Turb. Power. 132 (6):061505-061505. DOI: 10.1115/1.4000132. Yook, S.-J., and Pui, D. Y. H. 2005. Estimation of Penetration Efficiencies through NASA Sampling Lines, submitted to NASA Glenn Research Center. National Aeronautics and Space Administration. Cleveland, OH. Zeldovitch, Y. B. 1946. “The Oxidation of Nitrogen in Combustion Explosions.” Acta Physicochimica. 21: 577–628.

89 List of Data Products Two supplementary data products that accompany this report are available for download from the ACRP website http://www.trb.org/Publications/PubsACRPProjectReportsAll.aspx. 1. Spreadsheet containing emissions data “ACRP_02_54_emissions.xlsx” (Microsoft Excel.xlsx format).* i. The “Emissions” sheet containing average emission indices and fuel flows for each mea- sured aircraft. Recommended substitutions to current data, engine family averages, and upper limits are also included. These tables are reproduced in their entirety in Appendix P. ii. The “PlumesPublish” sheet contains emission indices for each measured test point. The included data are Engine ID, Engine Type, Plume Index, Engine State, Start Time, Stop Time, Fuel Flow, % of Max Fuel Flow, Percent of Max Propeller RPM or % of Max Rated Thrust for Turbos, EI CO, EI HC (as CH4), EI NOx (as NO2), EI PM # non-volatile (via APC), EI PM # Total (via EEPS), EI PM mass non-volatile (via MAAP), EI PM mass Total (via EEPS), EI CH4, EI C2H6, EI C2H4, EI C2H2, EI benzene, EI Toluene, EI C2benzenes, EI naphthalene, EI acetone, EI acetaldehyde, EI formaldehyde, EI BC via SP-AMS, EI Org via SP-AMS, EI PbTot via SP-AMS, ambient temperature, and ambient pressure. iii. The “FuelFlows” sheet contains constants for the exponential fit to fuel flow, as described in Appendix J. 2. Presentation summarizing key findings (Microsoft PowerPoint.pptx format) *Note that AEDT does not allow the saving of user-entered aircraft. Emissions indices and fuel flows reported in the Excel spreadsheet “Emissions” tab are appropriate for direct input into AEDT. A sample AEDT user-entered aircraft window is shown in Chapter 4, Sensitivity Analysis on Airport Emissions A P P E N D I X O