Gas Dynamics & Supersonic Flow
Compressible Flow
Equations of Motion
1-D Isentropic Flow
Wave Propogation
Nozzles and Ducts
2-D Compressible Flow
Prandtl-Meyer Expansions
Shock Interactions and Detached Shocks
Shock-Expansion Techniques for Aerofoils
Method of Characteristics
Unsteady Supersonic Flow
Molecular Simulation of Rarefied Flows
Compressible Flow Tables/Applications
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Sections :
- Compressible Flow
- System, Surroundings and Control Volume -- Laws of Thermodynamics -- Zeroth Law of Thermodynamics -- First Law of Thermodynamics
-- Second Law of Thermodynamics -- Perfect Gas Law -- Consequences of First Law for a Perfect Gas -- Consequences of Second Law for a Perfect Gas
- Equations of Motion for a Compressible Flow
- Continuity Equation -- Momentum Equation -- Energy Equation -- Stagnation Conditions -- Constant from Stagnation Conditions -- Area-Velocity Relation
- 1-D Isentropic Relations
- Sonic Point as Reference -- Mass Flow Rate -- Equations of Motion in absence of Area Changes
- Wave Propagation
- Speed of Sound -- Propagation of a Source of Sound -- Stationary Source -- Source moving at Subsonic Speeds -- Source moving at the Speed of Sound
-- Source moving at Supersonic Speeds -- Response of Subsonic and Supersonic Flows to an Obstacle -- Subsonic Flow -- Supersonic Flow -- Shock Waves
-- Formation of a Shock Wave -- Normal Shock Waves -- Important Characteristics of a Normal Shock
- Flow through Nozzles and Ducts
- Flow through a Converging Nozzle -- Flow through a Converging-diverging nozzle -- Supersonic Nozzle Flow Experiment
- Two-Dimensional Compressible Flow
- Oblique Shock Waves -- Relations across an Oblique Shock -- Relation between β and θ -- Supersonic Flow past Concave Corners and Wedges
-- Weak Oblique Shocks -- Supersonic Compression by Turning -- Convergence of Mach Waves
- Prandtl-Meyer Expansion
- Calculation of Downstream conditions
- Shock Interactions and Detached Shocks
- Shock Reflection from a Wall -- Intersection of two Shocks -- Strong Solutions – Detached Shocks -- Mach Reflection
- Shock-Expansion Techniques for Aerofoils
- Flat Plate Aerofoil -- Diamond Aerofoil -- Interaction between shocks and expansion waves -- Thin Aerofoil Theory -- Flow about a Flat Plate Aerofoil at an Angle of Attack
-- Diamond Aerofoil -- An Arbitrary Aerofoil -- Second Order Theory -- Reduction of Drag by cancelling the Waves
- Method of Characteristics
- Theory of Method of Characteristics -- Compatibility Relations -- Computing with Method of Characteristics -- Flow through a Diverging Duct -- Interior Point
-- Boundary Point -- Cancellation of Waves -- Design of a Supersonic Nozzle
- Unsteady Supersonic Flow
- Moving Normal Shock Waves -- Shock Induced Motion -- Reflection of a Moving Shock -- Unsteady Expansion Waves -- Shock Tube Flow
- Molecular Simulation of Rarefied Flow
- Transport Phase -- Collision Phase -- Flow Sampling -- Software and Exmaples
- Compressible Flow Tables/Software
- Subsonic Compressible Flow Table -- Supersonic Compressible Flow Table -- Normal Shock, Mach wave and Expansion Wave Table -- Oblique Shock Wave Table
-- Isentropic Compressible Flow Calculator -- Normal Shock Calculator -- Mach Wave Calculator -- Expansion Wave Calculator -- Oblique Shock Wave Calculator
-- Supersonic Nozzle Simulator -- Shocktube Simulator
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