A CFD Based Sonic Boom Prediction Method and Investigation on the Parameters Affecting the Sonic Boom Signature-Reference-Cited by-同舟云学术

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A CFD Based Sonic Boom Prediction Method and Investigation on the Parameters Affecting the Sonic Boom Signature

Published:2015 Issue: Volume:99 Page:433-451
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Lengyan ,Zhansen Qian

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference18 articles.

1. Sonic boom, chapter 10, aeroacoustics of flight vehicles[R];Maglieri;NASA RP-1258,1991

2. The Relation between Minimizing Drag and Noise at Supersonic Speeds, Proceedings, High Speed Aerodynamics;Busemann;Polytechnic Institute of Brooklyn,1955

3. Lower Bounds for Sonic Bangs;Jones;Journal of the Royal Aeronautical Society,1961

4. The Lower Bound of Attainable Sonic-Boom Overpressure and Design Methods of Approaching This Limit;Carlson;NASA TND-1494,1962

5. Influence of Airplane Configuration on Sonic Boom Characteristics;Carlson;J. Aircraft 1,1964

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. On the issue of optimizing the supersonic business aircraft layout in order to reduce sonic boom;Engineering Journal: Science and Innovation;2022-04

2. Application of Mathematical Modeling to Study Near-Field Pressure Pulsations of a Near-Future Prototype Supersonic Business Aircraft;Journal of Aerospace Engineering;2022-01

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