Application of a partitioned field approach to transient aerothermal problems in rocket nozzles

Author:

Hosters N.,Klaus M.,Behr M.,Reimerdes H.-G.

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference32 articles.

1. Forster C, Cowles F. Experimental study of gas-flow separation in overexpanded exhaust nozzles for rocket motors. Progress report, 4-103, Jet Propulsion Laboratory; 1949

2. Birken P, Quint KJ, Hartmann S, Meister Ai. On coupling schemes for heat transfer in FSI applications. In: Proceedings inter-workshop on fluid-structure interaction: theory, numerics and applications. Herrsching, Germany; 2009

3. Partitioned analysis of coupled mechanical systems;Felippa;Comput Meth Appl Mech Eng,2001

4. Load and motion transfer algorithms for fluid/structure interaction problems with non-matching discrete interfaces: momentum and energy conservation, optimal discretization and application to aeroelasticity;Farhat;Comput Meth Appl Mech Eng,1998

5. Conservative load transfer along curved fluid–solid interface with non-matching meshes;Jaiman;J Comput Phys,2006

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1. Conjugate Heat Transfer in High-Speed External Flows: A Review;Journal of Thermophysics and Heat Transfer;2023-10

2. Modified Method of Characteristics for Analysing Cold Flow in Bell-Type Rocket Nozzle;Lecture Notes in Mechanical Engineering;2020-11-22

3. Investigations of Base Thermal Environment on Four-Nozzle Liquid Launch Vehicle at High Altitude;Journal of Spacecraft and Rockets;2020-01

4. Applied and Theoretical Aspects of Conjugate Heat Transfer Analysis: A Review;Archives of Computational Methods in Engineering;2018-01-27

5. Fluid-Structure Interaction in the Context of a Scramjet Intake;44th AIAA Fluid Dynamics Conference;2014-06-13

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