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Sippel, Martin und Okai, Keiichi und Kato, Hiromasa und Kumar, Apurva (2007) Preliminary Definition of a TBCC Propulsion System for a Mach 4.5 Supersonic Cruise Airliner. ISABE 2007, 02.-07. Sep 2007, Beijing, China.
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Kurzfassung
The paper investigates different Variable Cycle TBCC configurations and compares them with an advanced turbojet for the generic configuration of a Mach 4.5 supersonic passenger airliner. One VCE engine variant and the turbojet are preliminarily designed and their mass including air-intake and nozzle is estimated. The airintake has been sized and pressure recovery and mass flow in design and off-design conditions is estimated and subsequently checked by the Navier-Stokes CFD code Argo.
| elib-URL des Eintrags: | https://elib.dlr.de/68084/ | ||||||||||||||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag, Paper) | ||||||||||||||||||||
| Titel: | Preliminary Definition of a TBCC Propulsion System for a Mach 4.5 Supersonic Cruise Airliner | ||||||||||||||||||||
| Autoren: |
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| Datum: | 2007 | ||||||||||||||||||||
| Open Access: | Ja | ||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||
| Stichwörter: | TBCC Propulsion System, Mach 4.5 Supersonic Cruise Airliner, turbine based cycle | ||||||||||||||||||||
| Veranstaltungstitel: | ISABE 2007 | ||||||||||||||||||||
| Veranstaltungsort: | Beijing, China | ||||||||||||||||||||
| Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
| Veranstaltungsdatum: | 02.-07. Sep 2007 | ||||||||||||||||||||
| Veranstalter : | AIAA - American Institute of Aeronautics and Astronautics, Inc. | ||||||||||||||||||||
| HGF - Forschungsbereich: | Verkehr und Weltraum (alt) | ||||||||||||||||||||
| HGF - Programm: | Weltraum (alt) | ||||||||||||||||||||
| HGF - Programmthema: | W RP - Raumtransport | ||||||||||||||||||||
| DLR - Schwerpunkt: | Weltraum | ||||||||||||||||||||
| DLR - Forschungsgebiet: | W RP - Raumtransport | ||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | W - Antriebsystemtechnik - Antriebskonzepte (alt) | ||||||||||||||||||||
| Standort: | Bremen | ||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Raumfahrtsysteme > Systemanalyse Raumtransport | ||||||||||||||||||||
| Hinterlegt von: | Zierenberg, Silke | ||||||||||||||||||||
| Hinterlegt am: | 10 Jan 2011 11:30 | ||||||||||||||||||||
| Letzte Änderung: | 31 Jul 2019 19:30 |
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