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Preliminary Definition of a TBCC Propulsion System for a Mach 4.5 Supersonic Cruise Airliner

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/
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:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Sippel, MartinSpace Launcher Systems Analysis (SART), DLR, 51170 Cologne, GermanyUNSPECIFIED
Okai, KeiichiAeroengine Technology Center, JAXA, JapanUNSPECIFIED
Kato, HiromasaNumerical Methods & Optimisation Group – CENAERO, 6041 Gosselies, BelgiumUNSPECIFIED
Kumar, ApurvaNumerical Methods & Optimisation Group – CENAERO, 6041 Gosselies, BelgiumUNSPECIFIED
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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