Work

A Simple Method for the Design of Supersonic Nozzles of Arbitrary Cross-Section Shape

Year: 2021

Type: other

DOI: 10.1115/1.0001617v

Authors: N Boughazi, A Haddad

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4242843752

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