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Simulations of Normal Shock-Wave/Boundary-Layer Interaction Control Using Mesoflaps
R. K. Jaiman, E. Loth,
J. C. Dutton
Aerospace Engineering
Mechanical Science and Engineering
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Keyphrases
Shock Wave Boundary Layer Interaction
100%
Stagnation Pressure
100%
Pressure Recovery
100%
Normal Shock Wave
100%
Interaction Control
100%
Deflection
50%
Boundary Layer Characteristics
50%
Mach number
25%
Low Pressure
25%
Pressure-driven Flow
25%
Steady State
25%
Flow Field
25%
Shock Waves
25%
Flap
25%
High-pressure Air
25%
Aeroelasticity
25%
Streamwise
25%
Normal Shock
25%
Lambda
25%
No Feedback
25%
Comparison with Experimental Results
25%
Turbulent Boundary Layers
25%
Passive Control
25%
Flat Wall
25%
State Deflection
25%
Characteristic Pressure
25%
Flap Deflection
25%
Cavity Depth
25%
Engineering
Boundary Layer
100%
Layer Interaction
100%
Normal Shock Wave
100%
Stagnation Pressure
100%
Pressure Recovery
100%
Flaps
50%
Streamwise
25%
Experimental Observation
25%
Experimental Result
25%
Pressure Flow
25%
Air Pressure
25%
Mach Number
25%
Turbulent Boundary Layer
25%