Unsteady Behavior of Long-Penetration Mode with a Counterflowing Jet-Reference-Cited by-同舟云学术

Unsteady Behavior of Long-Penetration Mode with a Counterflowing Jet

Published:2023-01 Issue:1 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Guo Xiaodong¹^ORCID,Zhou Chaoying²

Affiliation:

1. Ph.D. Candidate, School of Mechanical Engineering and Automation, Harbin Institute of Technology, Shenzhen 518055, China. ORCID: .

2. Professor, School of Mechanical Engineering and Automation, Harbin Institute of Technology, Shenzhen 518055, China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001497

Reference44 articles.

1. Adams R. H. and P. O. Jarvinen. 1970. “The effects of retrorockets on the aerodynamic characteristics of conical aeroshell planetary entry vehicles.” In Proc. 8th Aerospace Sciences Meeting. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-219.

2. Aso S. K. Hayashi and M. Mizoguchi. 2002. “A study on aerodynamic heating reduction due to opposing jet in hypersonic flow.” In Proc. 40th AIAA Aerospace Sciences Meeting & Exhibit. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-646.

3. Drag reduction of supersonic blunt bodies using opposing jet and nozzle geometric variations

4. Computational study of drag reduction at various freestream flows using a counterflow jet from a hemispherical cylinder;Bilal Hussain Shah S.;Eng. Appl. Comput. Fluid Mech.,2010

5. Candler, G. V., and I. Nompelis. 2009. Computational fluid dynamics for atmospheric entry. Minneapolis: Univ. of Minnesota.

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2. Behaviors of the long penetration mode with a hot counterflowing jet;Aerospace Science and Technology;2022-11