Time- and Length Scales of Combustion in Liquid Rocket Thrust Chambers

2002 ◽  
Vol 18 (2) ◽  
pp. 247-253 ◽  
Author(s):  
B. Ivancic ◽  
W. Mayer
Keyword(s):  
Length Scales ◽  
Rocket Thrust ◽  
Liquid Rocket

Film cooling modeling in liquid rocket thrust chambers

2021 ◽  
Author(s):  
Pierluigi Concio ◽  
Simone D'Alessandro ◽  
Mario Tindaro Migliorino ◽  
Francesco Nasuti
Keyword(s):  
Film Cooling ◽  
Rocket Thrust ◽  
Liquid Rocket

Numerical Investigation on Radiative Heat Loads in Liquid Rocket Thrust Chambers

2019 ◽  
Vol 35 (5) ◽  
pp. 930-943 ◽  
Author(s):  
Giuseppe Leccese ◽  
Daniele Bianchi ◽  
Francesco Nasuti
Keyword(s):  
Numerical Investigation ◽  
Radiative Heat ◽  
Rocket Thrust ◽  
Liquid Rocket ◽  
Heat Loads

A numerical model for coupling between atomization and spray dynamics in liquid rocket thrust chambers

1992 ◽  
Author(s):  
M. GIRIDHARAN ◽  
J. LEE ◽  
A. KRISHNAN ◽  
A. PRZEKWAS ◽  
KLAUS GROSS
Keyword(s):  
Numerical Model ◽  
Rocket Thrust ◽  
Liquid Rocket

scholarly journals Consequences of modeling demands on numerical rocket thrust chamber flow simulation tools

2019 ◽  
Author(s):  
O. Knab ◽  
H. Riedmann ◽  
B. Ivancic ◽  
C. Höglauer ◽  
M. Frey ◽  
...  
Keyword(s):  
Flow Simulation ◽  
Time Frame ◽  
Computational Effort ◽  
Full Scale ◽  
Test Cases ◽  
Thrust Chamber ◽  
Simulation Tools ◽  
Rocket Thrust ◽  
Liquid Rocket ◽  
Model Features

Numerical simulation of liquid rocket thrust chamber flows is a challenging task which requires a comprehensive tool validation strategy encompassing laboratory- to full-scale test cases. While the former are widely used as the first step to verify advanced numerical schemes and thermochemical models, the latter can often no more be simulated in a reasonable time frame due to the extreme computational effort necessitated by the enlarged dimensions and configurational changes. Conclusions drawn from tools with such limitations are only of little help for a thrust chamber designer and, hence, ill-posed to adequately tackle the simulation challenges of such a device. This paper discusses the modeling demands for numerical thrust chamber flow simulation tools and outlines the indispensable validation approach from laboratory- via subto full-scale configurations using consistent model features throughout the test cases. Consequences of this obligation are exposed to drive the tool setup. Exemplarily, the Airbus DS thrust chamber flow simulation philosophy is presented.

Convective and Radiative Wall Heat Transfer in Liquid Rocket Thrust Chambers

2018 ◽  
Vol 34 (2) ◽  
pp. 318-326 ◽  
Author(s):  
Giuseppe Leccese ◽  
Daniele Bianchi ◽  
Barbara Betti ◽  
Diego Lentini ◽  
Francesco Nasuti
Keyword(s):  
Heat Transfer ◽  
Wall Heat Transfer ◽  
Rocket Thrust ◽  
Liquid Rocket
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