The Calorimeter Nozzle Programme
Stark, R. and Hagemann, G. and Alting, J. and Kretschmer, J. and Terhardt, M. and Frey, M. and Ryden, R. (2002) The Calorimeter Nozzle Programme. In: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, IN. AIAA. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, IN, 7 - 10 July 2002.
Full text not available from this repository.
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 (Paper)|
|Additional Information:||LIDO-Berichtsjahr=2003, monograph_id=AIAA 2002-3998,|
|Title:||The Calorimeter Nozzle Programme|
|Journal or Publication Title:||38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, IN|
|Event Title:||38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, IN, 7 - 10 July 2002|
|Organizer:||American Institute of Aeronautics and Astronautics (AIAA)|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Space|
|HGF - Program Themes:||W RP - Raumtransport|
|DLR - Research area:||Space|
|DLR - Program:||W RP - Raumtransport|
|DLR - Research theme (Project):||E -- no assignement|
|Institutes and Institutions:||Institute of Space Propulsion|
|Deposited By:||Monika Lohmiller|
|Deposited On:||16 Sep 2005|
|Last Modified:||06 Jan 2010 14:00|
Repository Staff Only: item control page