Update search
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
NARROW
Format
Journal
Type
Date
Availability
1-2 of 2
Keywords: Hypersonic flow
Close
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
Sort by
Journal Articles
CFD investigation of shock boundary layer interaction in hypersonic flow and flow control using micro ramps
Available to Purchase
Aircraft Engineering and Aerospace Technology: An International Journal (2022) 94 (6): 862–870.
Published: 21 January 2022
... in hypersonic flow. Figure 3 Fluid domain with ramp setup The computational domain is meshed using tetrahedral elements and a sphere zone of influence is perceived near the ramp area with an element size of 2 mm for precisely capturing the boundary layer as shown in Figure 4 . Inflation layer were...
Journal Articles
Effects of boundary‐layers bleeding on performance parameters of hypersonic inlets
Available to Purchase
Aircraft Engineering and Aerospace Technology: An International Journal (2009) 81 (3): 204–211.
Published: 15 May 2009
... Limited 2009 Boundary layers Hypersonic flow Performance testing δi=angle of the wedge li=length of the wedge H=height of the isoloator k=turbulent kinetic energy ε=turbulent dissipation...
