Reynolds number and wind tunnel wall effects on the flow field around a generic UHBR engine high-lift configuration
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
-
1869-5590
- Extent
-
Online-Ressource
- Language
-
Englisch
- Notes
-
online resource.
- Bibliographic citation
-
Reynolds number and wind tunnel wall effects on the flow field around a generic UHBR engine high-lift configuration ; day:31 ; month:8 ; year:2020 ; pages:1-15
CEAS Aeronautical Journal / Confederation of European Aerospace Societies ; (31.8.2020), 1-15
- Creator
-
Ullah, Junaid
Prachař, Aleš
Šmíd, Miroslav
Seifert, Avraham
Soudakov, Vitaly
Lutz, Thorsten
Krämer, Ewald
- Contributor
-
SpringerLink (Online service)
- DOI
-
10.1007/s13272-020-00463-w
- URN
-
urn:nbn:de:101:1-2020101820104418160202
- Rights
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
14.08.2025, 10:51 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
- Ullah, Junaid
- Prachař, Aleš
- Šmíd, Miroslav
- Seifert, Avraham
- Soudakov, Vitaly
- Lutz, Thorsten
- Krämer, Ewald
- SpringerLink (Online service)
Other Objects (12)
Reynolds number and wind tunnel wall effects on the flow field around a generic UHBR engine high-lift configuration
Numerical parameter study of a strake on a Turboprop engine in active high-lift configuration
Numerical Investigation of a Generic Scramjet Configuration
Experiment Design for a Distributed Propulsion Configuration at High Lift
A generic accounting configuration architecture for multi-service mobile networks
Numerical investigations of vortex formation on a generic multiple-swept-wing configuration
E-Mails von Reynolds, Reynold
Total Facelift: Forehead Lift, Midface Lift, and Neck Lift
Reynolds
Investigation and Optimisation of High-Lift Airfoils for Airborne Wind Energy Systems at High Reynolds Numbers
LIFT
Joshua Reynolds
Reynolds number and wind tunnel wall effects on the flow field around a generic UHBR engine high-lift configuration
Numerical parameter study of a strake on a Turboprop engine in active high-lift configuration
Numerical Investigation of a Generic Scramjet Configuration
Experiment Design for a Distributed Propulsion Configuration at High Lift
A generic accounting configuration architecture for multi-service mobile networks
Numerical investigations of vortex formation on a generic multiple-swept-wing configuration
E-Mails von Reynolds, Reynold
Total Facelift: Forehead Lift, Midface Lift, and Neck Lift
Reynolds
Investigation and Optimisation of High-Lift Airfoils for Airborne Wind Energy Systems at High Reynolds Numbers
LIFT
Joshua Reynolds
Reynolds number and wind tunnel wall effects on the flow field around a generic UHBR engine high-lift configuration
Numerical parameter study of a strake on a Turboprop engine in active high-lift configuration
Numerical Investigation of a Generic Scramjet Configuration
Experiment Design for a Distributed Propulsion Configuration at High Lift
A generic accounting configuration architecture for multi-service mobile networks
Numerical investigations of vortex formation on a generic multiple-swept-wing configuration
E-Mails von Reynolds, Reynold
Total Facelift: Forehead Lift, Midface Lift, and Neck Lift
Reynolds
Investigation and Optimisation of High-Lift Airfoils for Airborne Wind Energy Systems at High Reynolds Numbers
LIFT