Keyphrases
Nozzle
100%
Hypersonic
100%
Arc-heated Wind Tunnel
100%
Flow Characterization
100%
Condensation
40%
Stagnation Temperature
40%
Pitot Pressure
40%
Flow Regions
20%
Root Mean Square
20%
Frequency up
20%
Flow Field
20%
Combustion
20%
Mach number
20%
Nozzle Exit
20%
Uniform Flow
20%
Axial Length
20%
Flow Regime
20%
Pressure Transducer
20%
Supersonic Flow
20%
Stagnation Pressure
20%
Static Pressure
20%
Angularity
20%
Hypersonic Wind Tunnel
20%
Flow Quality
20%
Pitot
20%
Spectral Content
20%
University of Notre Dame
20%
Hypersonic Flow
20%
Pressure Probe
20%
Engineering
Stagnation Temperature
100%
Pressure Sensor
100%
Mach Number
50%
Nozzle Exit
50%
Uniform Flow
50%
Flow Regime
50%
Flow Region
50%
Stagnation Pressure
50%
Supersonic Flow
50%
Exit Plane
50%
Static Pressure
50%
Pressure Probe
50%
Angularity
50%
Hypersonic Flows
50%
Flow Distribution
50%