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Numerical investigation of supersonic nozzle flow separation
Q. Xiao
, H.M. Tsai, D. Papamoschou
Naval Architecture, Ocean And Marine Engineering
Research output
:
Contribution to journal
›
Article
›
peer-review
95
Citations (Scopus)
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Dive into the research topics of 'Numerical investigation of supersonic nozzle flow separation'. Together they form a unique fingerprint.
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Engineering
Flow in Nozzles
100%
Flow Separation
100%
Asymmetric Flow
50%
Convergent
50%
Expansion Ratio
50%
Lambda Shock
25%
Nozzle Pressure
25%
Compression Wave
25%
Throat Area Ratio
25%
Wall-Pressure
25%
Flow Separate
25%
Reynolds-Averaged Navier-Stokes
25%
Earth and Planetary Sciences
Supersonic Nozzle
100%
Nozzle Flow
100%
Compression Wave
50%
Convergent-Divergent Nozzle
50%
Turbulence Model
25%
Flow Structure
25%
Wave Phenomena
25%
Supersonic Flow
25%
Pressure Ratio
25%
Succession
25%
Physics
Nozzle Flow
100%
Supersonics
100%
Supersonic Flow
50%
Elastic Wave
50%
Turbulence Model
25%
Wave Phenomena
25%
Throats
25%
Wall Pressure
25%