Hannemann, Klaus und Martinez Schramm, Jan und Viguier, Paul und Defoort, Sebastien und Steelant, Johan (2015) Experimental Comparative Synthesis on the Scramjet Powered Waverider Vehicle in HEG and F4 within the LAPCAT II project. 8th European Symposium on Aerothermodynamics for Space Vehicles, 2015-03-02 - 2015-03-06, Lisbon, Portugal.
Dieses Archiv kann nicht den Volltext zur Verfügung stellen.
Offizielle URL: http://www.congrexprojects.com/Custom/15A01/Index.html
Kurzfassung
The experimental measurements on a complex, hydrogen fuelled, 1.5 m long Mach 8 scramjet powered flight experiment configuration consisting of intake, combustor and thrust nozzle will be reported in this paper. The outer mold line of this small scale flight configuration (SSFE) was derived from the full scale Mach 8 cruiser MR 2 proposed by ESA-ESTEC within the EC co-funded LAPCAT II project. In the framework of LAPCAT II [21], the two major European free jet facilities, the High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center (DLR) and the F4 hot shot facility of the French Aerospace Lab (ONERA) were used to perform these measurements. The main emphasis of the tests in HEG and F4 is placed on Mach 8 flight conditions. The paper will give an experimental synthesis on both campaigns and discuss the complementary results in both facilities.
elib-URL des Eintrags: | https://elib.dlr.de/93580/ | ||||||||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||
Zusätzliche Informationen: | http://www.congrexprojects.com/Custom/15A01/Papers/Room%202.2/Tuesday/Propulsion%20Modelling%20I/90042_MartinezSchramm.pdf | ||||||||||||||||||||||||
Titel: | Experimental Comparative Synthesis on the Scramjet Powered Waverider Vehicle in HEG and F4 within the LAPCAT II project | ||||||||||||||||||||||||
Autoren: |
| ||||||||||||||||||||||||
Datum: | 2015 | ||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||
Seitenbereich: | Seiten 1-8 | ||||||||||||||||||||||||
Name der Reihe: | Conference Proceedings online | ||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||
Stichwörter: | ultra-fast, high enthalpy, force measurements, scramjets | ||||||||||||||||||||||||
Veranstaltungstitel: | 8th European Symposium on Aerothermodynamics for Space Vehicles | ||||||||||||||||||||||||
Veranstaltungsort: | Lisbon, Portugal | ||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||
Veranstaltungsbeginn: | 2 März 2015 | ||||||||||||||||||||||||
Veranstaltungsende: | 6 März 2015 | ||||||||||||||||||||||||
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 - Raumfahrzeugsysteme - Anlagen u. Messtechnik (alt) | ||||||||||||||||||||||||
Standort: | Göttingen | ||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Raumfahrzeuge | ||||||||||||||||||||||||
Hinterlegt von: | Micknaus, Ilka | ||||||||||||||||||||||||
Hinterlegt am: | 05 Mai 2015 11:41 | ||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:59 |
Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags