Technical Abstract Bulletin PDF Download
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Author:
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ISBN:
Category : Science
Languages : en
Pages : 368
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 368
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Author:
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ISBN:
Category : Power resources
Languages : en
Pages : 332
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Author:
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ISBN:
Category : Pollution
Languages : en
Pages : 490
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Author:
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ISBN:
Category : Science
Languages : en
Pages : 198
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Author:
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ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 942
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 296
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Author: Tara I. Yacovitch
Publisher:
ISBN: 9780309446013
Category : Aircraft exhaust emissions
Languages : en
Pages : 10
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Background -- Research approach -- Trends in emission indices -- Sensitivity analysis on airport emissions -- Other parameters affecting emissions -- Conclusions -- Appendix A: Engine prioritization list -- Appendix B: Test matrix -- Appendix C: ICAO vs. FOCA databases -- Appendix D: Method for calculating emission ratios -- Appendix E: Method for calculating emission ratios -- Appendix F: Variability in emissions results from variability in the engine -- Appendix G: Gas-phase measurement instrument -- Appendix H: PM measurement instruments -- Appendix I: PM line losses -- Appendix J: Estimating fuel flows for piston engines -- Appendix K: Carbon content of AVGAS 100 LL -- Appendix L: Hypothetical airport engine mapping -- Appendix M: Terminology and abbreviations -- Appendix N: References -- Appendix O: List of data products -- Appendix P: Emission index data tables
Author: National Research Council (U.S.). Committee on Aeronautical Technologies
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ISBN:
Category : Aeronautics
Languages : en
Pages : 21
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Author: K. M. Morrison
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ISBN:
Category : Airplanes
Languages : en
Pages : 118
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The primary purpose of this extensive test effort was to observe real-time operational performance characteristics associated with automotive grade fuel utilized by piston engine powered light general aviation aircraft. In fulfillment of this effort, baseline engine operations were established with 100LL aviation grade fuel followed by four blends of automotive grade fuel. A comprehensive - sea - level - static test cell/flight test data collection and evaluation effort was conducted to review operational characteristics of a carburated light aircraft piston engine as related to fuel volatility, fuel temperature, and fuel system pressure. Sea - level - static test cell engines operations were conducted utilizing an AVCO Lycoming 0-320 engine connected to an eddy current dynamometer which facilitated data collection under various engine load conditions. In addition, real-time inflight performance data was obtained utilizing a Cessna 150/Continental 0-200A engine, while operating on test fuels No. 1 and No. 2 which had Reid vapor pressures of 14.4 psi and 8.0 psi, respectively. Originator furnished key words include: General Aviation, Automotive Fuel, Aviation Fuel, Vapor lock, Vapor-Liquid Ratio, Fuel Additives, Light Aircraft, Piston Engines, and Fuel Volatility.
Author:
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ISBN:
Category : Airplanes
Languages : en
Pages : 20
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