- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
-
1432-1114
- Extent
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Online-Ressource
- Language
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Englisch
- Notes
-
online resource.
- Bibliographic citation
-
Experiments on a smooth wall hypersonic boundary layer at Mach 6 ; volume:59 ; number:4 ; day:22 ; month:3 ; year:2018 ; pages:1-21 ; date:4.2018
Experiments in fluids ; 59, Heft 4 (22.3.2018), 1-21, 4.2018
- Classification
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Ingenieurwissenschaften und Maschinenbau
- Creator
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Neeb, Dominik
- Contributor
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Saile, Dominik
Gülhan, Ali
SpringerLink (Online service)
- DOI
-
10.1007/s00348-018-2518-z
- URN
-
urn:nbn:de:101:1-2018062023343422599873
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
15.08.2025, 7:34 AM CEST
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Neeb, Dominik
- Saile, Dominik
- Gülhan, Ali
- SpringerLink (Online service)
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Notes on the hypersonic boundary layer transition
Research Progress of hypersonic boundary layer transition control experiments
Characterization of a hypersonic turbulent boundary layer along a sharp cone with smooth and transverse square−bar roughened wall
Numerical simulation of turbulent shock boundary layer interactions in hypersonic flows
Controlling hypersonic boundary layer transition with localized cooling and metasurface treatments
Experimental investigations of hypersonic boundary layer transition on a re-entry capsule
Effects of discrete roughness elements on laminar-turbulent transition in a hypersonic boundary layer
Oblique-mode breakdown in hypersonic and high-enthalpy boundary layers over a blunt cone
Wall pressure beneath a transitional hypersonic boundary layer over an inclined straight circular cone
Passive hypersonic boundary layer transition control using ultrasonically absorptive carbon-carbon ceramic with random microstructure
Roughness-Induced Transition in a Hypersonic Capsule Boundary Layer under Wind-Tunnel and Reentry Conditions
On the drag reduction mechanism of hypersonic turbulent boundary layers subject to heated wall blowing
Notes on the hypersonic boundary layer transition
Research Progress of hypersonic boundary layer transition control experiments
Characterization of a hypersonic turbulent boundary layer along a sharp cone with smooth and transverse square−bar roughened wall
Numerical simulation of turbulent shock boundary layer interactions in hypersonic flows
Controlling hypersonic boundary layer transition with localized cooling and metasurface treatments
Experimental investigations of hypersonic boundary layer transition on a re-entry capsule
Effects of discrete roughness elements on laminar-turbulent transition in a hypersonic boundary layer
Oblique-mode breakdown in hypersonic and high-enthalpy boundary layers over a blunt cone
Wall pressure beneath a transitional hypersonic boundary layer over an inclined straight circular cone
Passive hypersonic boundary layer transition control using ultrasonically absorptive carbon-carbon ceramic with random microstructure
Roughness-Induced Transition in a Hypersonic Capsule Boundary Layer under Wind-Tunnel and Reentry Conditions