Work

Design concept of compression wave and opposite cowl shock configuration for hypersonic inlet with inward deflecting cowl

Year: 2025

Type: article

Source: Physics of Fluids

DOI: 10.1063/5.0297492

Authors: Xue-bin Tang, Jia Cai, Zai-jie Liu, He-xia Huang, Yuan Qin, Kun Wang, Hui-jun Tan, Ye Tian

Institutions: Nanjing University of Aeronautics and Astronautics, Shenzhen Technology University

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: National Natural Science Foundation of China

Awards: G4233734745, G6336693799

OpenAlex ID: W4417039145

FWCI: 0.447

Cites: 34

Cited by: 1

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