Publikationen

2024
Flow fields around asymmetrical micro vortex generators in supersonic flow[DOI]
Hristozova, Lilia; Sebastian, Robin; Schreyer, Anne-Marie
Aerospace science and technology 145 108838 (2024)
Design considerations for efficient spanwise-inclined air-jet vortex generators for separation control in supersonic and hypersonic flows[DOI]
Sebastian, Robin; Schreyer, Anne-Marie
Aerospace science and technology 147 109033 (2024)
A region-segmentation combinational loss model based on data-driven machine learning for a boundary layer ingestion fan[DOI]
Pan, Tianyu; Shi, Kaikai; Lu, Hanan; Yang, Zhe; Zhang, Jian; Li, Qiushi
Aerospace science and technology 144 108780 (2024)
2020
Flow field around a spanwise-inclined jet in supersonic crossflow[DOI]
Sebastian, Robin; Lürkens, Thomas; Schreyer, Anne-Marie
Aerospace science and technology 106 106209 (2020)
Analysis of a drag reduced flat plate turbulent boundary layer via uniform momentum zones[DOI]
Li, Wenfeng; Roggenkamp, Dorothee; Paakkari, Ville; Klaas, Michael; Soria, Julio; Schröder, Wolfgang
Aerospace science and technology 96 105552 (2020)
2019
Influence of spanwise transversal surface wave on coherent structures in turbulent boundary layers[DOI]
Roggenkamp, Dorothee; Li, Wenfeng; Klaas, Michael; Schröder, Wolfgang
Aerospace science and technology 86 387-400 (2019)
2004
Experimental investigation of a pitched airfoil in transonic flow[DOI]
Hillenherms, Cornelia; Schröder, Wolfgang; Limberg, Wolfram
Aerospace science and technology 8-7 583-590 (2004)
Investigation of the engine jet/wing tip vortex interference[DOI]
Huppertz, Guido; Fares, Ehab Mahmoud Aziz Mohamed; Abstiens, Ronald; Schröder, Wolfgang
Aerospace science and technology 8-3 175-183 (2004)
2003
Investigation of engine jet/wing-tip vortex interference
Fares, Ehab Mahmoud Aziz Mohamed; Huppertz, Guido; Abstiens, Ronald; Schröder, Wolfgang
Aerospace science and technology 8-3 175-183 (2003)