Peter Jang Email & Phone Number

Currently supporting NASA JSC directly with CFD on HyperSTEP/CobraMRV assessing heating on the flaps as they get deflected into the flow and push the shock out using two-temperature model for 5-spcies air. Additionally, trying to assess RCS placement options to help ensure JE (Jet Effectiveness) at these hypersonic conditions.Chemically reacting CFD supporting rocket plume induced heating and impingement to shock refinement and interactions, including SRP (Supersonic Retro Propulsion) on Commercial Crew Program as well as Orion Program.Experienced in DPLR, OVERFLOW, Loci-CHEM, LAURA, and DAC (DSMC Analysis Code).Rocket engine plume/firing simulation and interaction on vehicle-to-vehicle and impingement.Worked on Boeing's CCDev/CCTS aerodynamics and CFD work with and without plume, ascent, ascent abort, and entry in generating CFD-based aerodatabase for GN&C and Loads internal customers running 1000's of casesSpecialty studies including different fairing sizes, lengthening the vehicles, different canting of jetsSupport wind tunnel tests to calibrate CFD accuracy as well as validating TSM model (Transition Sensitive Model) for short blunt vehicle application including real-time data analysis.Worked on CEV (Constellation program) LAV (Launch Abort Vehicle) CFD work for NASA using OVERFLOW.Shuttle Windows OML change database using OVERFLOWData extraction/post-processing using Linux shell scripts, awk, sed and other toolsHydrogen leak/flammability analysis, Space Shuttle aerodynamics database, Boundary Layer data extraction.High altitude rarefied flow aerodynamics using DAC (DSMC Analysis Code) including plume expansion and distribution in vacuum.Pre-flight and post-flight Shuttle data analysis along with developing, maintaining and providing tools to deliver critical Shuttle-related data.=======================================Boeing Frontiers Magazinehttp://www.boeing.com/news/frontiers/archive/2010/february/i_bds03.pdfNASA Publications:Effect of Abort Motor Thrust Offset on AM Jet Interaction using OVERFLOW, EG-CAP-AR-91, 2009ALAS-11 Rev 3 ACM Assessment Using OVERFLOW, EG-CAP-07-114, 2007ALAS-11 Rev 3 ACM Assessment Using OVERFLOW – Altitude Effects and Thrust Ratio Scaling Assessment, EG-CAP-07-121, 2007Rendezvous and Proximity Operations Design Reference (RPODR) for the International Space Station, Rev. D, 2001Specialties: DPLR, OVERFLOW, Loci-CHEM, LAURA, DAC, and Fluent, MADCAP, FieldView 12, Tecplot 360

Listed skills include Aerodynamics, Cfd, Ansys, Tecplot, and 21 others.