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Ian A. Waitz
Researcher at Massachusetts Institute of Technology
Publications - 139
Citations - 6607
Ian A. Waitz is an academic researcher from Massachusetts Institute of Technology. The author has contributed to research in topics: Combustor & Combustion chamber. The author has an hindex of 45, co-authored 139 publications receiving 6188 citations. Previous affiliations of Ian A. Waitz include University of Cambridge & California Institute of Technology.
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Transport impacts on atmosphere and climate: Metrics
Jan S. Fuglestvedt,Keith P. Shine,Terje Koren Berntsen,Jolene Cook,David S. Lee,Andrea Stenke,Ragnhild Bieltvedt Skeie,Guus J. M. Velders,Ian A. Waitz +8 more
TL;DR: In this article, the authors present Global Warming Potentials (GWPs) as these have traditionally been used in the implementation of climate policy, and discuss the uncertainties in these estimates, and the ranking of the various components with respect to their confidence in the given metric values is also given.
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Air pollution and early deaths in the United States. Part I: Quantifying the impact of major sectors in 2005
TL;DR: In this article, a multiscale air quality model is applied to assess the health impacts of major emissions sectors in United States and the results indicate the extent to which policy measures could be undertaken in order to mitigate the impact of specific emissions from different sectors d in particular black carbon emissions from road transportation and sulfur dioxide emissions from power generation.
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Historical and future trends in aircraft performance, cost, and emissions
TL;DR: In this paper, the authors analyzed the historical influence of aircraft performance on cost to examine the potential pace of future efficiency improvements and emissions reduction, and quantified and correlated the technological and operational influences on aircraft energy intensity.
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A six-wafer combustion system for a silicon micro gas turbine engine
TL;DR: In this article, the authors present the design, fabrication, packaging, and experimental test results for the 6-wafer combustion system for a silicon microengine, which is largely fabricated by deep reactive ion etching through a total thickness of 3800 /spl mu/m.
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Combustors for micro-gas turbine engines
TL;DR: In this paper, a hydrogen-air microcombustor is proposed for use in a 1 mm 2 inlet area, micro-gas turbine engine, and the entire combustion process is carried out at temperatures below the limitations set by material properties, resulting in a significant reduction of complexity when compared to larger scale gas turbine combustors.