Robust Low-Boom Design Based on Near-Field Pressure Signature in Whole Boom Carpet
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Tokyo 181-0015, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C033972
Reference21 articles.
1. Sonic boom minimization including both front and rear shocks
2. Sonic Boom Theory: Its Status in Prediction and Minimization
3. Ground Data Collection of Shaped Sonic Boom Experiment Aircraft Pressure Signatures
4. Boom Minimization Framework for Supersonic Aircraft Using CFD Analysis
5. Interactive Inverse Design Optimization of Fuselage Shape for Low-Boom Supersonic Concepts
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