Shaping a Supersonic Passenger Aircraft with Minimal Sonic Boom

Methods for reducing the shock wave produced by supersonic passenger aircraft are considered. Aerodynamic contouring of the aircraft to reduce the boom is proposed. A method is developed for assessing the proposed contours in the early design stages.

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Publication Details

Journal
Russian Engineering Research
Published
2025-03-01
DOI
https://doi.org/10.3103/s1068798x25700236
Citations
2
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
Field-Weighted Citation Impact
2.67
Controls
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article

Shaping a Supersonic Passenger Aircraft with Minimal Sonic Boom

R. Kh. Arifullin, S.A. Serebryanskiy, S. N. Shkarubo
2 citations
Russian Engineering Research
Computational Fluid Dynamics and Aerodynamics
2.67
article

Shaping a Supersonic Passenger Aircraft with Minimal Sonic Boom

R. Kh. Arifullin, S.A. Serebryanskiy, S. N. Shkarubo
article en
2 citations

Abstract

Methods for reducing the shock wave produced by supersonic passenger aircraft are considered. Aerodynamic contouring of the aircraft to reduce the boom is proposed. A method is developed for assessing the proposed contours in the early design stages.

Russian Engineering ResearchVol. 45(3)
Moscow Aviation Institute (RU)
Affordable and clean energy
Openalex Percentile: Top 12%
Computational Fluid Dynamics and Aerodynamics
2.67
DOISourceOpenAlex
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Shaping a Supersonic Passenger Aircraft with Minimal Sonic Boom — R. Kh. Arifullin, S.A. Serebryanskiy, et al. · Russian Engineering Research (2025) | TGRS Research Map | TGRS