Multifidelity Uncertainty Quantification of a Commercial Supersonic Transport
Authors:
- 1 May 2020
- journal article
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 57 (3) , 491-500
Abstract
The objective of this work was to develop a multifidelity uncertainty quantification approach for efficient analysis of a commercial supersonic transport concept. An approach based on point-colloca...Keywords
Funding Information
- Langley Research Center
This publication has 45 references indexed in Scilit:
- Nearfield Summary and Statistical Analysis of the Second AIAA Sonic Boom Prediction WorkshopJournal of Aircraft, 2019
- Summary and Statistical Analysis of the First AIAA Sonic Boom Prediction WorkshopJournal of Aircraft, 2016
- Summary of the 2008 NASA Fundamental Aeronautics Program Sonic Boom Prediction WorkshopJournal of Aircraft, 2014
- Sonic-Boom Mitigation Through Aircraft Design and Adjoint MethodologyJournal of Aircraft, 2014
- Adaptive Aft Signature Shaping of a Low-Boom Supersonic Aircraft Using Off-Body Pressures2012
- Adjoint-based low-boom design with Cart3D (Invited)2011
- Parallel Adjoint Framework for Aerodynamic Shape Optimization of Component-Based Geometry2011
- Supersonic drag reduction technology in the scaled supersonic experimental airplane project by JAXAProgress in Aerospace Sciences, 2009
- Quiet Spike Near Field Flight Test Pressure Measurements with CFD Comparisons2008
- Origins and Overview of the Shaped Sonic Boom Demonstration Program2005