Multi-objective, Multidisciplinary Optimization of Low-Boom Supersonic Transports Using Multifidelity Models-Reference-Cited by-同舟云学术

Multi-objective, Multidisciplinary Optimization of Low-Boom Supersonic Transports Using Multifidelity Models

Published:2022-09 Issue:5 Volume:59 Page:1137-1151
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Li Wu¹,Geiselhart Karl¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Funder

Aeronautics Research Mission Directorate

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036656

Reference58 articles.

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4. WelgeH.BonetJ.MageeT.TompkinsD.BrittT.NelsonC.MillerG.StensonD.StaubachJ.BalaN.DugeR.O’BrienM.CedozR.BarlowA.MartinsS.ViarsP.RasheedA.KirbyM.RaczynskiC.RoughenK.DoyleS.AlstonK.PageJ.PlotkinK. “N+3 Advanced Concept Studies for Supersonic Commercial Transport Aircraft Entering Service in the 2030-2035 Period,” NASA CR-2011-217084, April 2011.

5. The flow pattern of a supersonic projectile

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