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Vision 2030 Aircraft Propulsion Grand Challenge Problem: Full-engine CFD Simulations with High Geometric Fidelity and Physics Accuracy2014 NASA published the outcome of the 2030 CFD (Computational Fluid Dynamics) Vision study: “CFD Vision 2030: A path to Revolutionary Computational Aerosciences” . The study provided a comprehensive review of the state of the art of CFD in 2014 for aerospace applications including, but not limited to, numerical algorithms, physics models, MDAO (Multidisciplinary Design Analysis and Optimization) and HPC (High Performance Computing) hardware. The study also proposed four conceptual ideas of Grand Challenge problems that would build on and benefit from advances outlined in the roadmap. The proposed challenges were meant to foster more detailed descriptions of grand challenge problems for specific disciplines. One of the proposed challenges was in the gas turbine propulsion area, focusing on transient full engine simulations. The current paper addresses detailed technical aspects of that challenge, and proposes a plan to approach it in a gradual manner, which includes high fidelity modeling of components, component coupling, and targeted experimental campaigns relying on common research models.
Document ID
20205011252
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
M S Anand
(Raytheon (United States) Waltham, Massachusetts, United States)
Gorazd Medic
(Raytheon (United States) Waltham, Massachusetts, United States)
Umesh Paliath
(Raytheon (United States) Waltham, Massachusetts, United States)
Ken Suder
(Glenn Research Center Cleveland, Ohio, United States)
Mujeeb Malik
(Langley Research Center Hampton, Virginia, United States)
Greg Laskowski
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
December 8, 2020
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: AIAA Scitech
Location: Virtual
Country: US
Start Date: January 11, 2021
End Date: January 21, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 698154.01.03.10.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
turbine engine
compressor
combustor
turbine
CFD
LES
RANS
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