Supersonic Technology Concept Aeroplanes for Environmental Studies
Author(s) -
Jeffrey J. Berton,
Dennis L. Huff,
Karl Geiselhart,
Jonathan Seidel
Publication year - 2020
Publication title -
aiaa scitech 2022 forum
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2020-0263
Subject(s) - turbofan , supersonic speed , takeoff , aeronautics , jet noise , aerospace engineering , aircraft noise , jet engine , environmental science , jet (fluid) , takeoff and landing , civil aviation , airplane , engineering , aviation , automotive engineering , computer science , noise reduction , artificial intelligence
The International Civil Aviation Organization is considering new environmental standards for future supersonic civil aircraft. NASA is supporting this effort by analyzing several notional, near-term supersonic transports. NASA’s performance, noise, and exhaust emission predictions for these transports are being used to inform a larger study that will determine the global environmental and economic impact of adding supersonic aircraft to the fleet beginning this decade. A supersonic business jet with a maximum takeoff gross weight of 55 tonnes is the focus of this paper. A smaller business jet weighing 45 tonnes is also discussed. Both airplanes use supersonic engines derived from a common contemporary commercial subsonic turbofan core. Aircraft performance, airport-vicinity noise, and exhaust emissions are predicted using NASA tools. Also investigated are some of the anticipated behaviors and requirements of these aircraft in the commercial airspace. The sensitivity of noise to system uncertainties is presented and alternative engine studies are discussed.
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