Sonic-Boom Mitigation Through Aircraft Design and Adjoint Methodology-Reference-Cited by-同舟云学术

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Sonic-Boom Mitigation Through Aircraft Design and Adjoint Methodology

Published:2014-03 Issue:2 Volume:51 Page:502-510
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Rallabhandi Sriram K.¹,Nielsen Eric J.²,Diskin Boris³

Affiliation:

1. National Institute of Aerospace, Hampton, Virginia 23666

2. Computational AeroSciences Branch, NASA Langley Research Center, Hampton, Virginia 23681

3. Mechanical and Aerospace Engineering Department, National Institute of Aerospace, Hampton, Virginia 23666

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032189

Reference27 articles.

1. Sonic boom minimization including both front and rear shocks

2. Sonic boom reduction through aircraft design and operation

3. Sonic‐Boom Minimization

4. Origins and Overview of the Shaped Sonic Boom Demonstration Program

5. Development of the Gulfstream Quiet Spike TM for Sonic Boom Minimization

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1. Discrete Adjoint Optimization Method for Low-Boom Aircraft Design Using Equivalent Area Distribution;Aerospace;2024-07-03

2. Recent progress of efficient low-boom design and optimization methods;Progress in Aerospace Sciences;2024-04

3. Recent Enhancements to Modeling Sonic Boom Propagation using Augmented Burgers' Equation;AIAA AVIATION 2023 Forum;2023-06-08

4. Deep learning for inverse design of low-boom supersonic configurations;Advances in Aerodynamics;2023-04-01

5. Goal-Oriented Discretization Error Control in Coupled Nearfield-Farfield Low-Boom Simulations;AIAA AVIATION 2022 Forum;2022-06-20

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