Modeling the Rapid Boil-Off of a Cryogenic Liquid When Injected into a Low Pressure CavityMany launch vehicle cryogenic applications require the modeling of injecting a cryogenic liquid into a low pressure cavity. The difficulty of such analyses lies in accurately predicting the heat transfer coefficient between the cold liquid and a warm wall in a low pressure environment. The heat transfer coefficient and the behavior of the liquid is highly dependent on the mass flow rate into the cavity, the cavity wall temperature and the cavity volume. Testing was performed to correlate the modeling performed using Thermal Desktop and Sinda Fluint Thermal and Fluids Analysis Software. This presentation shall describe a methodology to model the cryogenic process using Sinda Fluint, a description of the cryogenic test set up, a description of the test procedure and how the model was correlated to match the test results.
Document ID
20160010321
Acquisition Source
Kennedy Space Center
Document Type
Presentation
Authors
Lira, Eric (a.i. Solutions, Inc. Kennedy Space Center, FL, United States)
Date Acquired
August 12, 2016
Publication Date
August 1, 2016
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
KSC-E-DAA-TN34363Report Number: KSC-E-DAA-TN34363
Meeting Information
Meeting: NASA Thermal Fluids & Analysis Workshop (TFAWS 2016)