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Further Validation of a CFD Code for Calculating the Performance of Two-Stage Light Gas GunsEarlier validations of a higher-order Godunov code for modeling the performance of two-stage light gas guns are reviewed. These validation comparisons were made between code predictions and experimental data from the NASA Ames 1.5" and 0.28" guns and covered muzzle velocities of 6.5 to 7.2 km/s. In the present report, five more series of code validation comparisons involving experimental data from the Ames 0.22" (1.28" pump tube diameter), 0.28", 0.50", 1.00" and 1.50" guns are presented. The total muzzle velocity range of the validation data presented herein is 3 to 11.3 km/s. The agreement between the experimental data and CFD results is judged to be very good. Muzzle velocities were predicted within 0.35 km/s for 74% of the cases studied with maximum differences being 0.5 km/s and for 4 out of 50 cases, 0.5 - 0.7 km/s.
Document ID
20170011636
Acquisition Source
Ames Research Center
Document Type
Technical Memorandum (TM)
Authors
Bogdanoff, David W.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Date Acquired
December 11, 2017
Publication Date
September 1, 2017
Subject Category
Spacecraft Design, Testing And Performance
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN44410
NASA/TM-2017-219571
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Ballistic Range
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