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Exploring Shock Wave–Boundary Layer Interaction Using Rainbow Schlieren Deflectometry

Year: 2024

Type: article

Source: SAE International Journal of Aerospace

DOI: 10.4271/01-18-01-0002

Authors: Narendra Datta, Semih Olcmen, Pankaj Kolhe

Institutions: University of West Alabama, University of Alabama

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4406161833

FWCI:

Cites: 38

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Related to: 10