Work

Hypersonic boundary layer flow at an axisymmetric stagnation point on a blunt body

Year: 2025

Type: article

Source: International Journal of Turbo and Jet Engines

DOI: 10.1515/tjj-2024-0109

Authors: Mahesh Kumari, Rama Subba Reddy Gorla

Institutions: Indian Institute of Science Bangalore, Wright-Patterson Air Force Base, U.S. Air Force Institute of Technology

Language: English

Topic: Gas Dynamics and Kinetic Theory

Subfield: Applied Mathematics

Field: Mathematics

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4408673034

FWCI:

Cites: 8

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Related to: 10