Application of Mathematical Modeling to Study Near-Field Pressure Pulsations of a Near-Future Prototype Supersonic Business Aircraft-Reference-Cited by-同舟云学术

Application of Mathematical Modeling to Study Near-Field Pressure Pulsations of a Near-Future Prototype Supersonic Business Aircraft

Published:2022-01 Issue:1 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Kozelkov A. S.¹,Strelets D. Yu.²^ORCID,Sokuler M. S.³,Arifullin R. H.³

Affiliation:

1. Head of Department of Computational Fluid Dynamics and Heat Transfer, Russian Federal Nuclear Center, Sarov, Nizhny Novgorod Region 607188, Russia.

2. Candidate of Technical Sciences, Head of R&D, Dept. of Aircraft Design and Certification, Moscow Aviation Institute (National Research Univ.), Moscow 125993, Russia. (corresponding author). ORCID: .

3. Senior Researcher, Dept. of Aircraft Design and Certification, Moscow Aviation Institute (National Research Univ.), Moscow 125993, Russia.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001373

Reference27 articles.

1. Carpenter F. L. and P. G. A. Cizmas. 2020. “UNS3D simulations for the third sonic boom prediction workshop part II: C608 low-boom flight demonstrator.” In Proc. AIAA AVIATION 2020 Forum. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2733.

2. Chernyshev, S. L. 2011. Sonic boom. Moscow: Nauka.

3. Computational Methods for Fluid Dynamics

4. Fletcher, C. A. J. 1991. Vol. II of Computational techniques for fluid dynamics, Vols. I, II. 2nd ed., 493. New York: Springer.

5. Methods for the Accurate Computations of Hypersonic Flows

Cited by 13 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. A Numerical Approach and Study of the Shock-Wave Structure of Supersonic Jet Flow in a Nozzle;Fluids;2024-07-18

2. Construction of a digital model and analysis of the characteristics of the air intake of the advanced supersonic passenger aircraft;AIP Conference Proceedings;2024

3. Comprehensive set of measures to optimize the layout of supersonic business aircraft to reduce sonic boom;AIP Conference Proceedings;2024

4. Modeling Object Motion on Arbitrary Unstructured Grids Using an Invariant Principle of Computational Domain Topology: Key Features;Symmetry;2023-11-17

5. Numerical Study of the Influence of the Critical Reynolds Number on the Aerodynamic Characteristics of the Wing Airfoil;Fluids;2023-10-13