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, 02.-07. Sep 2007, 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 Dates: | 02.-07. Sep 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: | 31 Jul 2019 19:30 |
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