NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Formulation and Implementation of Inflow/Outflow Boundary Conditions to Simulate Propulsive EffectsNo abstract available
Document ID
20180002422
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Rodriguez, David L.
(Science and Technology Corp. Moffett Field, CA, United States)
Aftosmis, Michael
(NASA Ames Research Center Moffett Field, CA, United States)
Nemec, Marian
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
April 17, 2018
Publication Date
January 8, 2018
Subject Category
Fluid Mechanics And Thermodynamics
Spacecraft Propulsion And Power
Report/Patent Number
ARC-E-DAA-TN51324
Meeting Information
Meeting: 2018 AIAA SciTech Forum
Location: Kissimmee, FL
Country: United States
Start Date: January 8, 2018
End Date: January 12, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA16BD60C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Boundary
Inflow/Outflow
Propulsive
No Preview Available