↓ Skip to main content

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

Overview of attention for book
Cover of 'Future Space-Transport-System Components under High Thermal and Mechanical Loads'

Table of Contents

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

Mentioned by

wikipedia
1 Wikipedia page

Citations

dimensions_citation
3 Dimensions

Readers on

mendeley
3 Mendeley
You are seeing a free-to-access but limited selection of the activity Altmetric has collected about this research output. Click here to find out more.
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
Authors

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%