Ponchio Camillo, Giannino und Wagner, Alexander und Dittert, Christian und Benjamin, Leroy und Wartemann, Viola und Neumann, Jens und Hink, Rüdiger (2020) Experimental investigation of the effect of transpiration cooling on second mode instabilities in a hypersonic boundary layer. Experiments in Fluids, 61 (162), Seiten 1-19. Springer Nature. doi: 10.1007/s00348-020-02994-8. ISSN 0723-4864.
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Offizielle URL: https://link.springer.com/article/10.1007/s00348-020-02994-8
Kurzfassung
The influence of localized nitrogen transpiration on second mode instabilities in a hypersonic boundary layer is experimentally investigated. The study is conducted using a 7deg half-angle cone with a length of 1100 mm and small nose bluntness at 0deg angle of attack. Transpiration is realized through a porous Carbon/Carbon patch of 44×82 mm located near the expected boundary layer transition onset location. Transpiration mass flow rates in the range of 0.05–1% of the equivalent boundary layer edge mass flow rate were used. Experiments were conducted in the High Enthalpy Shock Tunnel Göttingen (HEG) at total enthalpies around 3 MJ/kg and unit Reynolds numbers in the range of 1.4e6 to 6.4e6 1/m. Measurements were conducted by means of coaxial thermocouples, Atomic Layer Thermopiles (ALTP), pressure transducers and high-speed schlieren. The present study shows that the most amplified second mode frequencies were shifted to lower values as nitrogen is transpired into the boundary layer. In some cases the instability amplitudes were found to be significantly reduced. The observed frequency reduction was verified to correlate with the change of the relative sonic line height in the boundary layer. The amplitude damping was observed to occur only until the most amplified frequencies were reduced to around 50% of their undisturbed values. When transpiration within this limit was performed shortly upstream of the natural boundary layer transition onset, a transition delay of approximately 17% could be observed.
elib-URL des Eintrags: | https://elib.dlr.de/135429/ | ||||||||||||||||||||||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||||||||||||||
Titel: | Experimental investigation of the effect of transpiration cooling on second mode instabilities in a hypersonic boundary layer | ||||||||||||||||||||||||||||||||
Autoren: |
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Datum: | 27 Juni 2020 | ||||||||||||||||||||||||||||||||
Erschienen in: | Experiments in Fluids | ||||||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||||||
Open Access: | Ja | ||||||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||||||||||||||
In ISI Web of Science: | Ja | ||||||||||||||||||||||||||||||||
Band: | 61 | ||||||||||||||||||||||||||||||||
DOI: | 10.1007/s00348-020-02994-8 | ||||||||||||||||||||||||||||||||
Seitenbereich: | Seiten 1-19 | ||||||||||||||||||||||||||||||||
Herausgeber: |
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Verlag: | Springer Nature | ||||||||||||||||||||||||||||||||
ISSN: | 0723-4864 | ||||||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||||||
Stichwörter: | hypersonic boundary layer, second mode instability, hypersonic transition, transpiration cooling, HEG, transition delay, porous surface, gas injection | ||||||||||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||||||||||||||||||||||
HGF - Programmthema: | Raumtransport | ||||||||||||||||||||||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||||||||||||||||||
DLR - Forschungsgebiet: | R RP - Raumtransport | ||||||||||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Wiederverwendbare Raumfahrtsysteme (alt) | ||||||||||||||||||||||||||||||||
Standort: | Braunschweig , Göttingen , Stuttgart | ||||||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Raumfahrzeuge, GO Institut für Aerodynamik und Strömungstechnik > Raumfahrzeuge, BS Institut für Bauweisen und Strukturtechnologie > Raumfahrt - System - Integration Institut für Aeroelastik > Aeroelastische Simulation | ||||||||||||||||||||||||||||||||
Hinterlegt von: | Wagner, Alexander | ||||||||||||||||||||||||||||||||
Hinterlegt am: | 03 Jul 2020 10:06 | ||||||||||||||||||||||||||||||||
Letzte Änderung: | 23 Okt 2023 12:36 |
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