Effects of Engine Emissions from High-Speed Civil Transport Aircraft


Book Description

The AER two-dimensional chemistry-transport model is used to study the effect of supersonic and subsonic aircraft operation in the 2010 atmosphere on stratospheric ozone (O3). The results show that: (1) the calculated O3 response is smaller in the 2010 atmosphere compared to previous calculations performed in the 1980 atmosphere; (2) with the emissions provided, the calculated decrease in O3 column is less than 1 percent; and (3) the effect of model grid resolution on O3 response is small provided that the physics is not modified. Ko, Malcolm K. W. and Weisenstein, Debra K. and Sze, Nein Dak and Shia, Run-Lie and Rodriguez, Jose M. and Heisey, Curtis Unspecified Center...







High-Speed Civil Transport Study: Special Factors


Book Description

Studies relating to environmental factors associated with high speed civil transports were conducted. Projected total engine emissions for year 2015 fleets of several subsonic/supersonic transport fleet scenarios, discussion of sonic boom reduction methods, discussion of community noise level requirements, fuels considerations, and air traffic control impact are presented. Unspecified Center CIVIL AVIATION; NOISE POLLUTION; SUBSONIC AIRCRAFT; SUPERSONIC AIRCRAFT; TRANSPORT AIRCRAFT; AIR TRAFFIC CONTROL; AIRPORTS; EXHAUST EMISSION; FUELS; NOISE INTENSITY; SONIC BOOMS...




High-speed Civil Transport Study


Book Description







Procedure for Generating Global Atmospheric Engine Emissions Data from Future Supersonic Transport Aircraft. the 1990 High Speed Civil Transport Studies


Book Description

The input for global atmospheric chemistry models was generated for baseline High Speed Civil Transport (HSCT) configurations at Mach 1.6, 2.2, and 3.2. The input is supplied in the form of number of molecules of specific exhaust constituents injected into the atmosphere per year by latitude and by altitude (for 2-D codes). Seven exhaust constituents are currently supplied: NO, NO2, CO, CO2, H2O, SO2, and THC (Trace Hydrocarbons). An eighth input is also supplied, NO(x), the sum of NO and NO2. The number of molecules of a given constituent emitted per year is a function of the total fuel burned by a supersonic fleet and the emission index (EI) of the aircraft engine for the constituent in question. The EIs for an engine are supplied directly by the engine manufacturers. The annual fuel burn of a supersonic fleet is calculated from aircraft performance and economic criteria, both of which are strongly dependent on basic design parameters such as speed and range. The altitude and latitude distribution of the emission is determined based on 10 Intern. Air Transport Assoc. (IATA) regions chosen to define the worldwide route structure for future HSCT operations and the mission flight profiles. Sohn, R. A. and Stroup, J. W. Unspecified Center NAS1-18378; RTOP 537-01-31-01...




High-Speed Civil Transport Study


Book Description

A system study of the potential for a high-speed commercial transport has addressed technological, economic, and environmental constraints. Market projections indicate a need for fleets of transports with supersonic or greater cruise speeds by the year 2000 to 2005. The associated design requirements called for a vehicle to carry 250 to 300 passengers over a range of 5,000 to 6,000 nautical miles. The study was initially unconstrained in terms of vehicle characteristic, such as cruise speed, propulsion systems, fuels, or structural materials. Analyses led to a focus on the most promising vehicle concepts. These were concepts that used a kerosene-type fuel and cruised at Mach numbers between 2.0 to 3.2. Further systems study identified the impact of environmental constraints (for community noise, sonic boom, and engine emissions) on economic attractiveness and technological needs. Results showed that current technology cannot produce a viable high-speed civil transport; significant advances are required to reduce takeoff gross weight and allow for both economic attractiveness and environmental accepatability. Specific technological requirements were identified to meet these needs. Unspecified Center CIVIL AVIATION; ECONOMIC ANALYSIS; ENVIRONMENT EFFECTS; MARKETING; STRUCTURAL DESIGN; TRANSPORT AIRCRAFT; AIRCRAFT NOISE; EXHAUST EMISSION; HIGH SPEED...