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Nasa's Atmospheric Effects of Aviation Project

Nasa's Atmospheric Effects of Aviation Project PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721263493
Category :
Languages : en
Pages : 40

Book Description
During August 1-14, 1999, NASA's Atmospheric Effects of Aviation Project (AEAP) convened a workshop at the NASA Langley Research Center to try to determine why such a wide variation in aerosol emissions indices and chemical and physical properties have been reported by various independent AEAP-supported research teams trying to characterize the exhaust emissions of subsonic commercial aircraft. This workshop was divided into two phases, a laboratory phase and a field phase. The laboratory phase consisted of supplying known particle number densities (concentrations) and particle size distributions to a common manifold for the participating research teams to sample and analyze. The field phase was conducted on an aircraft run-up pad. Participating teams actually sampled aircraft exhaust generated by a Langley T-38 Talon aircraft at 1 and 9 m behind the engine at engine powers ranging from 48 to 100 percent. Results from the laboratory phase of this intercomparison workshop are reported in this paper. Cofer, W. Randy, III and Anderson, Bruce E. and Connors, V. S. and Wey, C. C. and Sanders, T. and Twohy, C. and Brock, C. A. and Winstead, E. L. and Pui, D. and Chen, Da-Ren Glenn Research Center; Langley Research Center NASA/TM-2001-210829, L-18063, NAS 1.15:210829

Nasa's Atmospheric Effects of Aviation Project

Nasa's Atmospheric Effects of Aviation Project PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721263493
Category :
Languages : en
Pages : 40

Book Description
During August 1-14, 1999, NASA's Atmospheric Effects of Aviation Project (AEAP) convened a workshop at the NASA Langley Research Center to try to determine why such a wide variation in aerosol emissions indices and chemical and physical properties have been reported by various independent AEAP-supported research teams trying to characterize the exhaust emissions of subsonic commercial aircraft. This workshop was divided into two phases, a laboratory phase and a field phase. The laboratory phase consisted of supplying known particle number densities (concentrations) and particle size distributions to a common manifold for the participating research teams to sample and analyze. The field phase was conducted on an aircraft run-up pad. Participating teams actually sampled aircraft exhaust generated by a Langley T-38 Talon aircraft at 1 and 9 m behind the engine at engine powers ranging from 48 to 100 percent. Results from the laboratory phase of this intercomparison workshop are reported in this paper. Cofer, W. Randy, III and Anderson, Bruce E. and Connors, V. S. and Wey, C. C. and Sanders, T. and Twohy, C. and Brock, C. A. and Winstead, E. L. and Pui, D. and Chen, Da-Ren Glenn Research Center; Langley Research Center NASA/TM-2001-210829, L-18063, NAS 1.15:210829