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Sippel, Martin and Okai, Keiichi and Kato, Hiromasa and Kumar, Apurva (2007) Preliminary Definition of a TBCC Propulsion System for a Mach 4.5 Supersonic Cruise Airliner. ISABE 2007, 2007-09-02 - 2007-09-07, Beijing, China.
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Abstract
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.
| Item URL in elib: | https://elib.dlr.de/68084/ | ||||||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech, Paper) | ||||||||||||||||||||
| Title: | Preliminary Definition of a TBCC Propulsion System for a Mach 4.5 Supersonic Cruise Airliner | ||||||||||||||||||||
| Authors: |
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| Date: | 2007 | ||||||||||||||||||||
| Open Access: | Yes | ||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||
| In SCOPUS: | No | ||||||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||
| Keywords: | TBCC Propulsion System, Mach 4.5 Supersonic Cruise Airliner, turbine based cycle | ||||||||||||||||||||
| Event Title: | ISABE 2007 | ||||||||||||||||||||
| Event Location: | Beijing, China | ||||||||||||||||||||
| Event Type: | international Conference | ||||||||||||||||||||
| Event Start Date: | 2 September 2007 | ||||||||||||||||||||
| Event End Date: | 7 September 2007 | ||||||||||||||||||||
| Organizer: | AIAA - American Institute of Aeronautics and Astronautics, Inc. | ||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport (old) | ||||||||||||||||||||
| HGF - Program: | Space (old) | ||||||||||||||||||||
| HGF - Program Themes: | W RP - Raumtransport | ||||||||||||||||||||
| DLR - Research area: | Space | ||||||||||||||||||||
| DLR - Program: | W RP - Raumtransport | ||||||||||||||||||||
| DLR - Research theme (Project): | W - Antriebsystemtechnik - Antriebskonzepte (old) | ||||||||||||||||||||
| Location: | Bremen | ||||||||||||||||||||
| Institutes and Institutions: | Institute of Space Systems > Space Launcher Systems Analysis | ||||||||||||||||||||
| Deposited By: | Zierenberg, Silke | ||||||||||||||||||||
| Deposited On: | 10 Jan 2011 11:30 | ||||||||||||||||||||
| Last Modified: | 24 Apr 2024 19:33 |
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