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Explores 2-dimensional modeling of supersonic flow over the wing. The general part of page - Java Applet. This package may help: 1. calculate and display the graphic of streamline over the wing 2. find thermo-aero-dynamic parameters of flow 3. control airfoil geometry in "real-time" mode 4. calculate and draw aerodynamic polar
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| URL: |
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| Title: |
Supersonic Wing |
| Description: |
Supersonic flow over the Wing |
| Category: |
Computational
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Software
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Dynamics
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Links
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Expansion
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Lift
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Modeling
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Fluid
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Wave
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Shock
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Picture
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Sound
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Simulator
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Mach
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Pressure
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Flow
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Modelling
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Supersonic
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Drag
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Java
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Intake
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Number
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Aerodynamics
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Wing
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Hypersonic
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Polar
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Aerodynamic
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Airfoil
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Inlet
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Joukowsky
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