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Optimal supersonic ejector designs
J. C. Dutton
, B. F. Carroll
Aerospace Engineering
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peer-review
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Keyphrases
Area Ratio
50%
Compression Ratio
50%
Design Curves
50%
Ejector
50%
Ejector Design
100%
Entrainment Ratio
50%
Flow Model
50%
Gas Properties
50%
Large Classes
50%
Optimization Problem
50%
Pressure Ratio
50%
Primary Nozzle
50%
Ratio Compression
50%
Stagnation Pressure
50%
Stagnation Temperature
100%
Supersonic Ejector
100%
Two-variable
50%
Engineering
Area Ratio
33%
Compression Ratio
33%
Dimensional Constant
33%
Ejector
100%
Entrainment Ratio
33%
Flow Model
33%
Molecular Weight
33%
One Dimensional
33%
Optimisation Problem
33%
Pressure Ratio
33%
Primary Nozzle
33%
Stagnation Pressure
33%
Stagnation Temperature
66%