Work

Design and Performance Analysis of Scramjet Inlet and Isolator Systems for Hypersonic Mach Regimes

Year: 2025

Type: article

Source: Fluid Dynamics

DOI: 10.1134/s001546282560227x

Authors: M. Stefaniya, S. Pushpalatha, A. R. Rajendran

Institutions: Noorul Islam University, Anna University, Chennai, Karunya University

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4416966140

FWCI:

Cites: 8

Cited by:

Related to: