2019•Aerospace Science and TechnologyRequires access

A proposed design method for supersonic inlet to improve performance parameters

Mohammad Farahani, M.M. Mahdavi

Open publisher page 25 citations

Abstract

This record does not include an abstract. Use the full-text link above if available.

About this research paper

What this paper is about

An abstract is not available in the OpenAlex record for this paper.

Why it matters

OpenAlex reports 25 citations for this work. Citation counts describe recorded attention and do not establish research quality.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Key concepts: Inlet, Supersonic speed, Mach number, Computational fluid dynamics, Mechanics, Aerospace engineering, Structural engineering, Mechanical engineering

Back to paper search Browse research topics Original source

A proposed design method for supersonic inlet to improve performance parameters — Research Paper | ScholarLens