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Future Space-Transport-System Components under High Thermal and Mechanical Loads

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Cover of 'Future Space-Transport-System Components under High Thermal and Mechanical Loads'

Table of Contents

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    Book Overview
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    Chapter 1 Collaborative Research for Future Space Transportation Systems
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    Chapter 2 A Coupled Two-Domain Approach for Transpiration Cooling
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    Chapter 3 Innovative Cooling for Rocket Combustion Chambers
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    Chapter 4 Film Cooling in Rocket Nozzles
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    Chapter 5 Numerical Simulation of Film Cooling in Supersonic Flow
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    Chapter 6 Heat Transfer in Pulsating Flow and Its Impact on Temperature Distribution and Damping Performance of Acoustic Resonators
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    Chapter 7 Effects of a Launcher’s External Flow on a Dual-Bell Nozzle Flow
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    Chapter 8 Interaction of Wake and Propulsive Jet Flow of a Generic Space Launcher
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    Chapter 9 Rocket Wake Flow Interaction Testing in the Hot Plume Testing Facility (HPTF) Cologne
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    Chapter 10 Numerical Analysis of the Turbulent Wake for a Generic Space Launcher with a Dual-Bell Nozzle
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    Chapter 11 Numerical Investigation of Space Launch Vehicle Base Flows with Hot Plumes
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    Chapter 12 On the Consideration of Diffusive Fluxes Within High-Pressure Injections
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    Chapter 13 Numerical Investigation of Injection, Mixing and Combustion in Rocket Engines Under High-Pressure Conditions
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    Chapter 14 Large-Eddy Simulations for the Wall Heat Flux Prediction of a Film-Cooled Single-Element Combustion Chamber
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    Chapter 15 Calculation of the Thermoacoustic Stability of a Main Stage Thrust Chamber Demonstrator
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    Chapter 16 Experimental Investigation of Injection-Coupled High-Frequency Combustion Instabilities
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    Chapter 17 Pseudo-transient 3D Conjugate Heat Transfer Simulation and Lifetime Prediction of a Rocket Combustion Chamber
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    Chapter 18 Lifetime Experiments of Regeneratively Cooled Rocket Combustion Chambers and PIV Measurements in a High Aspect Ratio Cooling Duct
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    Chapter 19 Mechanical Integrity of Thermal Barrier Coatings: Coating Development and Micromechanics
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    Chapter 20 Assessment of RANS Turbulence Models for Straight Cooling Ducts: Secondary Flow and Strong Property Variation Effects
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    Chapter 21 Experiments on Aerothermal Supersonic Fluid-Structure Interaction
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    Chapter 22 Numerical Modelling of Fluid-Structure Interaction for Thermal Buckling in Hypersonic Flow
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    Chapter 23 Experimental and Numerical Investigation of CH $$_4$$ /O $$_2$$ Rocket Combustors
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    Chapter 24 Rocket Combustion Chamber Simulations Using High-Order Methods
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    Chapter 25 Dual-Bell Nozzle Design
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    Chapter 26 Definition and Evaluation of Advanced Rocket Thrust Chamber Demonstrator Concepts
Attention for Chapter 25: Dual-Bell Nozzle Design
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Chapter title
Dual-Bell Nozzle Design
Chapter number 25
Book title
Future Space-Transport-System Components under High Thermal and Mechanical Loads
Published by
Springer, Cham, January 2021
DOI 10.1007/978-3-030-53847-7_25
Book ISBNs
978-3-03-053846-0, 978-3-03-053847-7

Chloé Génin, Dirk Schneider, Ralf Stark, Génin, Chloé, Schneider, Dirk, Stark, Ralf

Mendeley readers

The data shown below were compiled from readership statistics for 3 Mendeley readers of this research output. Click here to see the associated Mendeley record.

Geographical breakdown

Country Count As %
Unknown 3 100%

Demographic breakdown

Readers by professional status Count As %
Unknown 3 100%
Readers by discipline Count As %
Unknown 3 100%