Work

Compressible Boundary Layer Effects on Performance of Low Thrust Nozzle

Year: 2025

Type: article

Source: Journal of Aerospace Sciences and Technologies

DOI: 10.61653/joast.v77i2.2025.1073

Authors: Deepa Raj Mopuru, Nishanth Dongari, Srihari P

Institutions: Defence Research and Development Organisation, Defence Research and Development Laboratory, Indian Institute of Technology Hyderabad

Language: English

Topic: Rocket and propulsion systems research

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4410547372

FWCI:

Cites: 7

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Related to: 10