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Simulations of SSLV Ascent and Debris Transport PDF

2006·8.6 MB·English
by  RogersStuart
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Simulations of SSLV Ascent and Debris Transport Space Shuttle Return-To-Flight SSttuuaarrtt RRooggeerrss MMiicchhaaeell AAffttoossmmiiss RReeyynnaallddoo GGoommeezz SSccootttt MMuurrmmaann DDaarrbbyy VViicckkeerr WWiilllliiaamm CChhaann PPhhiill SSttuuaarrtt JJiimm GGrreeaatthhoouussee NNAASSAA AAddvvaanncceedd SSuuppeerrccoommppuuttiinngg DDiivviissiioonn NNAASSAA JJoohhnnssoonn SSppaaccee CCeenntteerr NNAASSAA AAmmeess RReesseeaarrcchh CCeenntteerr Seminar in Fluid Mechanics Stanford University October 11, 2005 1 Outline (cid:137)CFD simulations of the Space Shuttle Launch Vehicle ascent (cid:137)Debris transport analysis (cid:137)Debris aerodynamic modeling 2 CFD Analysis of SSLV Ascent Motivation (cid:137) Predict air-loads on the redesigned External Tank (cid:137) Roll maneuver air-loads (cid:137) Debris analysis flow-fields (cid:137) 3% Shuttle wind-tunnel test loads prediction Approach (cid:137) Overflow RANS flow solver (cid:190) Central-differencing + scalar dissipation, 2nd order (cid:190) Diagonalized approximate factorization implicit scheme (cid:190) Spalart-Allmaras turbulence model (cid:190) Multi-level parallelism, scalable to hundreds of CPUs (cid:190) Use full-multi-grid sequencing to get started (cid:137) Overset (Chimera) gridding approach (cid:190) Developed an automated grid-generation capability (cid:190) Gimble angles for SSME and SRB nozzles (cid:190) Control surface deflections (cid:190) Plume boundary-condition generation for SSMEs and SRBs (cid:137) Validation with 3% WT model: Cp, PSP, PIV 3 CFD Analysis of SSLV Ascent Results (cid:137)Over 400 Overflow solutions run for Return-to- Flight (cid:137)New grids generated for each ascent condition (cid:190) 2 hours on 32 Itanium-2 CPUs (cid:190) 30 to 50 million grid points each (cid:137)Average of ~1000 Itanium-2 CPU hrs / solution (cid:190) ~20 hours of wallclock time running on 64 Itanium-2 CPUs (cid:190) Never converges to a steady-state: aft end of ET, attachment hardware, plumes, etc (cid:190) Typically run for ~10,000 iterations 4 Geometry Details New Grids with New Grids without Bipod Ramp Bipod Ramp Control Surface and nozzle deflections 5 Old Grid System “Columbia”: World Class Supercomputing (cid:137) The NAS houses the world’s fastest operational supercomputer providing 61 teraflops of compute capability to the NASA user community (cid:137) Columbia is a 20-node supercomputer built on 512-processor nodes (cid:137) Columbia is the largest SGI system in the world with over 10,000 Intel Itanium2 processors 6 IA-700 Wind Tunnel Tests ARC 9x7 Unitary, AEDC 16T 7 IA-700 Transonic Surface Cp – Orbiter Wing 8 IA-700 Transonic Surface Cp – ET Stagnation pressure is artificially high in the PSP data because of poor camera angles 9 Integrated Wing Loads 10 J. Greathouse/JSC

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