2d and 3d Method of Characteristics for Nozzle Design

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Applied Physics Laboratory RTDC-TPS-48 I Laurel MD 207236099 Y 2D and 3D Method of Characteristic Tools for Complex Nozzle Development Final Report Tharen Rice June 3 0,2003 Prepared under Grant No. NAG3-2460, “Design of Exhaust Nozzle for the RBCC- GTX Concept,” with the NASA Glenn Research Center THE JOHNS HOPKINS UNIVERSITY APPLIED PHYSICS LABORATORY Johns Hopkins Road, Laurel, Maryland 20723-6099 1 J m HOpKINs OS U N I V B R S I T Applied PhytiCS Laboratory RTDC-TPS-48 1 Laurel M D 207236(199 Y Table of Contents 1 .0 Purpose .................................................................................................................. 2.0…show more content…
4.2 4.2.1 File Input/Output...................................................................................... 4.2.2 Grid Setup ................................................................................................ 4.2.3 Surface Fit ................................................................................................ 4.2.4 Initial Plane Properties ............................................................................. 4.2.5 Calculate Nozzle Button and Progress Indicators .................................... 4.2.6 Print Output Parameters ........................................................................... 5.0 2D and 3D MOC Tool Verification ...................................................................... 2D MOC Tool Verification ............................................................................... 5.1 3D MOC Tool Verification .............................................................................. 5.2 6.0 Summary............................................................................................................... 2 5 5 7 7 10 10 11 12 12 12 13 13 13 14 14 15 16 16 18 18 19 20 23 23 23 26 27 27 28 29 30 31 31 32 32 32 33 33 34 34 36 36 36 40 J O ~ HO~KINS Applied physics Laboratory S MD Laurel U N I V 7.0 8.0 9.0 B R S I T RTDC-TPS-48 1 20723-6099 Y References

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