Dataset of the experimentally measured heat transfer in the throat region of liquid rocket engine thrust chambers.

ABSTRACT: About 500 experimental heat transfer data taken from the open literature and relevant to the most thermally solicited area (i.e., the throat region) of liquid rocket engine thrust chambers, are collected and manipulated. This collection is the outcome of a thorough and exhaustive survey of the available experimental data of hot-fire tests produced to date. Among the test cases reported in the literature, only those with a throat heat transfer that is not affected by laminar flow, evident soot deposition, or intended non-uniform propellant injection are collected. The heat transfer is typically measured in terms of wall heat flux and temperature. Sometimes the heat transfer coefficient, which is a combination of these two terms, is provided. Each collected heat transfer measurement is suppl

SUBMITTER: Pizzarelli M 

PROVIDER: S-EPMC8187832 | biostudies-literature | 2021 Aug

REPOSITORIES: biostudies-literature