Leading-edge bluntness effects on hypersonic three-dimensional flows over a compression ramp
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Bibliographic citation
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In: 10.1017/jfm.2021.552
- Event
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Veröffentlichung
- (where)
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Aachen
- (who)
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Universitätsbibliothek der RWTH Aachen
- (when)
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2021
- Creator
- DOI
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10.18154/RWTH-2021-07615
- URN
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urn:nbn:de:101:1-2022061504451215170794
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
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15.08.2025, 7:31 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
- Cao, Shibin
- Hao, Jiaao
- Klioutchnikov, Igor
- Olivier, Herbert
- Heufer, Karl Alexander
- Wen, Chih-Yung
- Universitätsbibliothek der RWTH Aachen
Time of origin
- 2021
Other Objects (12)
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Stability of hypersonic flow over a curved compression ramp
Reattachment heating upstream of short compression ramps in hypersonic flow
Transition to turbulence in hypersonic flow over a compression ramp due to intrinsic instability
Occurrence of global instability in hypersonic compression corner flow
Perinatal computing: The leading edge
ILES of an array of three subsonic counter-flow jets issuing from a wing leading edge exposed to hypersonic aerodynamic heating
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Leading-edge flow criticality as a governing factor in leading-edge vortex initiation in unsteady airfoil flows
Leading-Edge Vortex Control by Unsteady Blowing
Ramp
Ramp
Streamwise vortices in hypersonic flow on a compression ramp
Stability of hypersonic flow over a curved compression ramp
Reattachment heating upstream of short compression ramps in hypersonic flow
Transition to turbulence in hypersonic flow over a compression ramp due to intrinsic instability
Occurrence of global instability in hypersonic compression corner flow
Perinatal computing: The leading edge
ILES of an array of three subsonic counter-flow jets issuing from a wing leading edge exposed to hypersonic aerodynamic heating
Deutschlands Spitzencluster : Germany's leading-edge clusters
Leading-edge flow criticality as a governing factor in leading-edge vortex initiation in unsteady airfoil flows
Leading-Edge Vortex Control by Unsteady Blowing
Ramp
Ramp
Streamwise vortices in hypersonic flow on a compression ramp
Stability of hypersonic flow over a curved compression ramp
Reattachment heating upstream of short compression ramps in hypersonic flow
Transition to turbulence in hypersonic flow over a compression ramp due to intrinsic instability
Occurrence of global instability in hypersonic compression corner flow
Perinatal computing: The leading edge
ILES of an array of three subsonic counter-flow jets issuing from a wing leading edge exposed to hypersonic aerodynamic heating
Deutschlands Spitzencluster : Germany's leading-edge clusters
Leading-edge flow criticality as a governing factor in leading-edge vortex initiation in unsteady airfoil flows
Leading-Edge Vortex Control by Unsteady Blowing
Ramp