Aerodynamic Interference Reduction Using Aerospike for Two-Stage Reusable Launch Vehicle-Reference-Cited by-同舟云学术

Aerodynamic Interference Reduction Using Aerospike for Two-Stage Reusable Launch Vehicle

Published:2023-07 Issue:4 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Liao Peng¹^ORCID,Song Wei²,Du Peng³^ORCID,Feng Feng²

Affiliation:

1. Ph.D. Candidate, Aerodynamics Science Center of China Academy of Aerospace Aerodynamics, China Academy of Aerospace Aerodynamics, Beijing 100074, China (corresponding author). ORCID: .

2. Associate Professor, Aerodynamics Science Center of China Academy of Aerospace Aerodynamics, China Academy of Aerospace Aerodynamics, Beijing 100074, China.

3. Associate Professor, School of Marine Science and Technology, Northwestern Polytechnical Univ., Xi’an 710072, China. ORCID: .

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/JAEEEZ.ASENG-4668

Reference19 articles.

1. Surrogate-Based Multi-Objective Aerothermodynamic Design Optimization of Hypersonic Spiked Bodies

2. Spike Effects on Drag Reduction for Hypersonic Lifting Body

3. Numerical study of shock wave and turbulent boundary layer interaction induced by flat-faced blunt fin;Deng X. G.;Chin. J. Theor. Appl. Mech.,1993

4. Investigation of Two-Stage-to-Orbit Airbreathing Launch-Vehicle Configurations

5. Iwafuji H. K. Masahiro and F. Takahiro. 2019. “Plume effect of flowfield around winged two-stage-to-orbit and its flight characteristics.” In Proc. AIAA Scitech 2019 Forum. Reston VA: American Institute of Aeronautics and Astronautics.

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. Unsteady interaction and dynamic stability analysis of a two-stage-to-orbit vehicle during transverse stage separation;Acta Astronautica;2024-03

2. Unsteady investigation on parallel separation for spiked two-stage reusable launch vehicle;Chinese Journal of Aeronautics;2023-11