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Computing measured spectra from hypersonic pitot probes with flow-parallel freestream disturbances
Ross S. Chaudhry,
Graham V Candler
Aerospace Engineering and Mechanics
Research output
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Contribution to journal
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Article
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peer-review
29
Scopus citations
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Dive into the research topics of 'Computing measured spectra from hypersonic pitot probes with flow-parallel freestream disturbances'. Together they form a unique fingerprint.
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Keyphrases
Hypersonic
100%
Transfer Function
100%
Measured Spectrum
100%
Freestream Disturbances
100%
Pitot Probe
100%
Disturbance Type
50%
Free Stream
50%
Shock
25%
Direct numerical Simulation
25%
Focusing Effect
25%
Resonant Frequency
25%
Analytic Form
25%
Pressure Spectrum
25%
Acoustic Disturbance
25%
Probe Geometry
25%
Stagnation Temperature
25%
Low-frequency Limit
25%
Shock Curvature
25%
Pitot Pressure
25%
Shock Stand-off Distance
25%
Engineering
Transfer Function
100%
Measured Spectrum
100%
Parallel Flow
100%
Single Curve
25%
Frequency Limit
25%
Stagnation Temperature
25%
Direct Numerical Simulation
25%
Resonant Frequency
25%