DLR Portal
Home|Textversion|Imprint|Sitemap|Contact |Deutsch
You are here: Home:Departments:Numerical Methods:Application
Advanced Search
News
Institute
Departments
Combustor
Combustion Test
Fan and Compressor
Numerical Methods
Research fields
Application
Publications
Simulationsystem
Projects
Engine
Engine Acoustics
Engine Measurement
Turbine
IT Infrastruktur
Facilities
Publications
Offers
Service & Links

Back to article

Validation of implicit non-reflecting boundary conditions: Upstream wave propagation (M = 0.4, Eta = 1.28, p0 = 89 Pa) Instantaneous pressure perturbation contours



Previous 2/8 Next
Validation of implicit non-reflecting boundary conditions: Upstream wave propagation (M = 0.4, Eta = 1.28, p0 = 89 Pa) Instantaneous pressure perturbation contours
Download this image: Hi-Res JPEG (0.04 MB)
Application
DLR-Institute of Propulsion Technology-Engine Acoustics Department
DLR-Institut für Lufttransportsysteme
Publications (elib)
Related Topics
Fluid Mechanics and Thermodynamics
Copyright © 2013 German Aerospace Center (DLR). All rights reserved.