Integration of Off-Track Sonic Boom Analysis for Supersonic Aircraft Conceptual Design
Author:
Affiliation:
1. Aeronautics Systems Analysis Branch, NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031511
Reference14 articles.
1. Quiet Spike Near Field Flight Test Pressure Measurements with CFD Comparisons
2. Efficient Unstructured Grid Adaptation Methods for Sonic Boom Prediction
3. Adjoint-Based Adaptive Mesh Refinement for Sonic Boom Prediction
4. Integration of Engine, Plume, and CFD Analyses in Conceptual Design of Low-Boom Supersonic Aircraft
5. A Mixed-Fidelity Approach for Design of Low-Boom Supersonic Aircraft
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1. Assessment of Off-Design Low-Boom Characteristics of a Low-Boom Supersonic Transport;AIAA SCITECH 2024 Forum;2024-01-04
2. Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport;Journal of Aircraft;2023-09-03
3. Redesign of a Low-Boom Supersonic Transport Using Powered Engine Simulation for Sonic Boom Analysis;AIAA SCITECH 2023 Forum;2023-01-19
4. Multi-objective, Multidisciplinary Optimization of Low-Boom Supersonic Transports Using Multifidelity Models;Journal of Aircraft;2022-09
5. Simplification of Numerical and Analytical Tools for Sonic Boom Description;Computational Mathematics and Mathematical Physics;2022-04
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