An Opportunity for Hydrogen Fueled Supersonic Airliners

This paper takes a new look at the prospects for developing supersonic civil airliners, considering global demographics, climate change issues, fuel prices and technological advances. Dramatic changes have occurred in the demographics, economics, and market intensity of the Eastern Hemisphere since...

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Main Authors: Alex Forbes, Anant Patel, Chris Cone, Pierre Valdez, Narayanan Komerath
Format: Article
Language:English
Published: International Institute of Informatics and Cybernetics 2011-02-01
Series:Journal of Systemics, Cybernetics and Informatics
Subjects:
Online Access:http://www.iiisci.org/Journal/CV$/sci/pdfs/NK814DZ.pdf
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spelling doaj-49ac2f99f78c4b97bb421fd0284a7c292020-11-24T21:57:51ZengInternational Institute of Informatics and CyberneticsJournal of Systemics, Cybernetics and Informatics1690-45242011-02-01915158An Opportunity for Hydrogen Fueled Supersonic AirlinersAlex Forbes0Anant Patel1Chris Cone2Pierre Valdez3Narayanan Komerath4 Georgia Institute of Technology Georgia Institute of Technology Georgia Institute of Technol Georgia Institute of Technology Georgia Institute of Technology This paper takes a new look at the prospects for developing supersonic civil airliners, considering global demographics, climate change issues, fuel prices and technological advances. Dramatic changes have occurred in the demographics, economics, and market intensity of the Eastern Hemisphere since the 1990s. Carbon reduction imperatives provide a major incentive to invest in developing hydrogen-fueled airliners. The “point-to-point” air route architecture has proved viable with long range mid-size airliners. With a cruise Mach number of 1.4, a large number of destinations become viable for overland supersonic flight. A conceptual design process is used to estimate cost per seat mile for a range of hydrocarbon and hydrogen fuel costs. An argument based on the ideal shape for minimal wave drag, estimates the drag penalty from using hydrogen. Viable aircraft geometries are shown to exist, that match the theoretical ideal shape, showing that the drag estimate is achievable. Conservative design arguments and market estimates suggest that hydrogen-fueled airliners can achieve seat-mile costs low enough to open a large worldwide market and justify a viable fleet size.http://www.iiisci.org/Journal/CV$/sci/pdfs/NK814DZ.pdf Wave DragDemographicsSeat Mile CostHydrogen Supersonic Airliner
collection DOAJ
language English
format Article
sources DOAJ
author Alex Forbes
Anant Patel
Chris Cone
Pierre Valdez
Narayanan Komerath
spellingShingle Alex Forbes
Anant Patel
Chris Cone
Pierre Valdez
Narayanan Komerath
An Opportunity for Hydrogen Fueled Supersonic Airliners
Journal of Systemics, Cybernetics and Informatics
Wave Drag
Demographics
Seat Mile Cost
Hydrogen Supersonic Airliner
author_facet Alex Forbes
Anant Patel
Chris Cone
Pierre Valdez
Narayanan Komerath
author_sort Alex Forbes
title An Opportunity for Hydrogen Fueled Supersonic Airliners
title_short An Opportunity for Hydrogen Fueled Supersonic Airliners
title_full An Opportunity for Hydrogen Fueled Supersonic Airliners
title_fullStr An Opportunity for Hydrogen Fueled Supersonic Airliners
title_full_unstemmed An Opportunity for Hydrogen Fueled Supersonic Airliners
title_sort opportunity for hydrogen fueled supersonic airliners
publisher International Institute of Informatics and Cybernetics
series Journal of Systemics, Cybernetics and Informatics
issn 1690-4524
publishDate 2011-02-01
description This paper takes a new look at the prospects for developing supersonic civil airliners, considering global demographics, climate change issues, fuel prices and technological advances. Dramatic changes have occurred in the demographics, economics, and market intensity of the Eastern Hemisphere since the 1990s. Carbon reduction imperatives provide a major incentive to invest in developing hydrogen-fueled airliners. The “point-to-point” air route architecture has proved viable with long range mid-size airliners. With a cruise Mach number of 1.4, a large number of destinations become viable for overland supersonic flight. A conceptual design process is used to estimate cost per seat mile for a range of hydrocarbon and hydrogen fuel costs. An argument based on the ideal shape for minimal wave drag, estimates the drag penalty from using hydrogen. Viable aircraft geometries are shown to exist, that match the theoretical ideal shape, showing that the drag estimate is achievable. Conservative design arguments and market estimates suggest that hydrogen-fueled airliners can achieve seat-mile costs low enough to open a large worldwide market and justify a viable fleet size.
topic Wave Drag
Demographics
Seat Mile Cost
Hydrogen Supersonic Airliner
url http://www.iiisci.org/Journal/CV$/sci/pdfs/NK814DZ.pdf
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