Work

Performance of Compound Angled Cooling Holes Within a Rotating Detonation Combustor

Year: 2026

Type: article

Source: Journal of Turbomachinery

DOI: 10.1115/1.4072583

Authors: Shreyas Ramanagar-Sridhara, Marc D. Polanka, Myles D. Bohon, Antonio Andreini

Institutions: University of Florence, U.S. Air Force Institute of Technology, Technische Universität Berlin

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W7203714376

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Cites: 25

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