Real gas effects in supersonic nozzles

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Title
Real gas effects in supersonic nozzles
CoPED ID
cd5561b5-d27f-46dd-a301-402ea8ffa1e7
Status
Closed
Funders
EPSRC
EPSRC
Value
No funds listed.
Start Date
Nov. 13, 2017
End Date
May 11, 2021
Description

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The project aims to numerically investigate the role played by the equation of state (EoS) on gas dynamics in a convergent-divergent nozzle. Considering an EoS representative of the behaviour of dense gases close to the thermodynamic critical point (a configuration occurring in ORC turbines for example), a variety of non-classical flow configurations (e.g. expansion shocks) can be observed. This project aims to explore some of these configurations and investigate their response to perturbations. Simulations will be carried out using the in-house compressible flow code CompReal.

Emile Touber SUPER_PER
Stephen Winn STUDENT_PER

Subjects by relevance
  1. Gases
  2. Simulation
  3. Dynamics

Extracted key phrases
  1. Real gas effect
  2. Dense gas close
  3. Gas dynamic
  4. Supersonic nozzle
  5. Classical flow configuration
  6. Divergent nozzle
  7. EoS representative
  8. House compressible flow code CompReal
  9. Thermodynamic critical point
  10. Project
  11. E.g. expansion shock
  12. Orc turbine

Related Pages

UKRI project entry

UK Project Locations