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

Authors

Mahesh Kumari, Indian Institute of Science, Bangalore
Rama Subba Reddy Gorla, Air Force Institute of TechnologyFollow

Document Type

Article

Publication Date

3-21-2025

Comments

Copyright © 2025 Walter de Gruyter GmbH, Berlin/Boston 2025.

This article paper is published online by de Gruyter as an article of International Journal of Turbo & Jet-Engines, ahead of inclusion in an issue of the journal.

DOI

10.1515/tjj-2024-0109

Source Publication

International Journal of Turbo & Jet-Engines (ISSN 0334-0082, 2191-0332)

Recommended Citation

Kumari, Mahesh and Gorla, Rama Subba Reddy. "Hypersonic boundary layer flow at an axisymmetric stagnation point on a blunt body" International Journal of Turbo & Jet-Engines, 2025. https://doi.org/10.1515/tjj-2024-0109