Uncertainty Analysis and Robust Design of Low-Boom Concepts Using Atmospheric Adjoints
Author:
Affiliation:
1. National Institute of Aerospace, Hampton, Virginia 23666
2. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C033908
Reference48 articles.
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4. MorgensternJ.NorstrudN.StelmackM.SkochC. “Final Report for the Advanced Concept Studies for Supersonic Commercial Transports Entering Service in the 2030 to 2035 Period, N+3 Supersonic Program,” NASA CR-2010-216796, Oct. 2010.
5. Adjoint-based method for supersonic aircraft design using equivalent area distribution
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