NASA Technical Reports Server (NTRS) 19950017199: Computational Fluid Dynamics (CFD) Analyses In Support Of Space Shuttle Main Engine (SSME) Heat Exchanger (HX) Vane Cracking Investigation - Info and Reading Options
By NASA Technical Reports Server (NTRS)
"NASA Technical Reports Server (NTRS) 19950017199: Computational Fluid Dynamics (CFD) Analyses In Support Of Space Shuttle Main Engine (SSME) Heat Exchanger (HX) Vane Cracking Investigation" and the language of the book is English.
“NASA Technical Reports Server (NTRS) 19950017199: Computational Fluid Dynamics (CFD) Analyses In Support Of Space Shuttle Main Engine (SSME) Heat Exchanger (HX) Vane Cracking Investigation” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19950017199: Computational Fluid Dynamics (CFD) Analyses In Support Of Space Shuttle Main Engine (SSME) Heat Exchanger (HX) Vane Cracking Investigation
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19950017199
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"NASA Technical Reports Server (NTRS) 19950017199: Computational Fluid Dynamics (CFD) Analyses In Support Of Space Shuttle Main Engine (SSME) Heat Exchanger (HX) Vane Cracking Investigation" Description:
The Internet Archive:
Integration issues involved with installing the alternate turbopump (ATP) High Pressure Oxygen Turbopump (HPOTP) into the SSME have raised questions regarding the flow in the HPOTP turnaround duct (TAD). Steady-state Navier-Stokes CFD analyses have been performed by NASA and Pratt & Whitney (P&W) to address these questions. The analyses have consisted of two-dimensional axisymmetric calculations done at Marshall Space Flight Center and three-dimensional calculations performed at P&W. These analyses have identified flowfield differences between the baseline ATP and the Rocketdyne configurations. The results show that the baseline ATP configuration represents a more severe environment to the inner HX guide vane. This vane has limited life when tested in conjunction with the ATP but infinite life when tested with the current SSME HPOTP. The CFD results have helped interpret test results and have been used to assess proposed redesigns. This paper includes details of the axisymmetric model, its results, and its contribution towards resolving the problem.
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