1968NASA STI Repository (National Aeronautics and Space Administration)Open access

Nonlinear combustion instability in liquid-propellant rocket motors Quarterly report

S. Z. Burstein, W. Chinitz

Open full text 0 citations

Abstract

Fluid dynamic pancake model and droplet evaporation and combustion analysis related to nonlinear combustion instability in liquid propellant rocket motors

Open-access reader

About this research paper

What this paper is about

Fluid dynamic pancake model and droplet evaporation and combustion analysis related to nonlinear combustion instability in liquid propellant rocket motors

Why it matters

A significance statement is not available in the OpenAlex record.

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.

Available abstract

Fluid dynamic pancake model and droplet evaporation and combustion analysis related to nonlinear combustion instability in liquid propellant rocket motors

Key concepts: Propellant, Liquid-propellant rocket, Rocket (weapon), Nonlinear system, Combustion, Instability, Aerospace engineering, Rocket propellant

Related papers

Back to paper searchBrowse research topicsOriginal source
Nonlinear combustion instability in liquid-propellant rocket motors Quarterly report — Research Paper | ScholarLens