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The Calorimeter Nozzle Programme

Hagemann, G. and Alting, J. and Kretschmer, J. and Terhardt, M. and Frey, M. and Ryden, R. and Stark, R. (2002) The Calorimeter Nozzle Programme. In: Proceedings of the 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 7. - 10. Jul. 2002, Indianapolis, USA.

Full text not available from this repository.

Abstract

When investigating flow phenomena in rocket nozzles, e.g. flow separation and side-load behavior for different nozzle concepts, or when experimentally screening design considerations for advanced nozzle concepts, the initial experimental effort is generally limited to subscale experiments with high quality diagnostics. But the fundamental question is how to scale these test results to a potential full-scale design or application, respectively. Different approaches exist, including the use of characteristic numbers for normalisation, analytical and numerical models.

Document Type:Conference or Workshop Item (Speech)
Additional Information:LIDO-Berichtsjahr=2003, monograph_id=AIAA 2002-3998,
Title:The Calorimeter Nozzle Programme
Authors:
AuthorsInstitution or Email of Authors
Hagemann, G.Astrium
Alting, J.Astrium
Kretschmer, J.Astrium
Terhardt, M.Astrium
Frey, M.Volvo Aero
Ryden, R.VOLVO Aero
Stark, R.Ralf.Stark@dlr.de
Date:2002
Journal or Publication Title:Proceedings of the 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Refereed publication:Yes
In ISI Web of Science:No
Publisher:AIAA
Status:Published
Keywords:rocket nozzles, flow separation
Event Title:38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Event Location:Indianapolis, USA
Event Type:international Conference
Event Dates:7. - 10. Jul. 2002
Organizer:American Institute of Aeronautics and Astronautics (AIAA)
HGF - Research field:Energy
HGF - Program:other
HGF - Program Themes:E - no assignment
DLR - Research area:Energy
DLR - Program:E - no assignment
DLR - Research theme (Project):E - no assignment
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Monika Lohmiller
Deposited On:16 Sep 2005
Last Modified:15 Feb 2016 08:13

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