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Using Global Market Demand Analysis to Guide Conceptual Design of Low-Boom Supersonic TransportsThis paper uses a mathematical framework to identify the interdependencies of key variables in supersonic transportation demand analysis. The existing quantitative models for supersonic transportation demand analysis are compared for consistency in modeling the interdependencies. Unlike other quantitative models, the Low-Boom Systems Analysis Model (LBSAM2) can propagate important design characteristics of a supersonic transport aircraft concept to the level of economic metrics (such as the number of future supersonic passengers), with a consistent coupling of the market demand analysis, detailed mission analysis, and low-boom constraint. This allows the use of the detailed demand analysis results from LBSAM2 to maximize the economic viability of a supersonic transport aircraft by finding favorable system-level trades between weight, range, fuel burn, and assumed sonic boom ground noise limit for supersonic overland flight. In this paper, LBSAM2 is integrated with conceptual low-boom design to improve the economic viability of low-boom supersonic transport aircraft. A brief discussion of uncertainties in the LBSAM2 analysis is also included, focusing on their impacts on the relative economic advantages between low-boom concepts.
Document ID
20240013705
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Wu Li
(Langley Research Center Hampton, Virginia, United States)
Karl Geiselhart
(Langley Research Center Hampton, Virginia, United States)
Ryan Palma
(Langley Research Center Hampton, United States)
Michael Patterson
(Langley Research Center Hampton, United States)
Samuel Dollyhigh
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Zhou Wang
(Virginia Tech Blacksburg, United States)
Nicolas Hinze
(Virginia Tech Blacksburg, United States)
Antonio Trani
(Virginia Tech Blacksburg, United States)
Date Acquired
October 29, 2024
Subject Category
Aircraft Design, Testing and Performance
Aeronautics (General)
Meeting Information
Meeting: AIAA SciTech Forum 2025
Location: Orlando, FL
Country: US
Start Date: January 6, 2025
End Date: January 10, 2025
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
TASK: NNL13AA08B
CONTRACT_GRANT: TDN-RSES.C2.10.00340
WBS: 090265.01.01.07.04
WBS: 110076.02.07.03.33
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
Consistent coupling of disciplinary analyses
Low-boom supersonic transport
Reversed equivalent area
Low-boom constraint
Supersonic market demand
Trade method for low-boom concept
Model-based analysis
Uncertainty assessment
Equilibrium state of supersonic market
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