1.introduction some basic concepts - virginia techdevenpor/aoe5104/1. introduction.pdf3a. ideal flow...
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1.Introduction Some Basic Concepts
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1.What is a fluid?
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2. What Properties Do Fluids Have?
• Density• Pressure • Temperature • Viscosity• Velocity • Compressibility
http://www.xcor.com/products/engines/5M15_LOX-Methane_rocket_engine.html
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Fourier’s Law of Heat Conduction
Newton’s Law of ViscosityU
y
nq
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3. What Constrains Fluid Motion?
Vanguard Class Submarine
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Two Important ParametersRate of change of = momentum (inertial force)
NACA 0012 Airfoil, Re = 1000000, M ~ 0Large Eddy SimulationInstitute of Computational Fluid DynamicsJapan
Sum of pressure forces, viscous forces and body forces
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3a. Ideal Flow Viscous and compressible effects small (large Re, low M). Flow is a balance between inertia and pressure forces, i.e. acceleration
vector balances the pressure gradient vector
Streamline:
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3a. Viscous Flow
What is the pressure gradient across a boundary layer?
Re=1000000Importance of viscous effects governed by
VL
Re
No-slip condition:
Boundary layer:
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3b Viscous FlowViscous region not always confined to a thin layer
Separation:
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Separation and Wake FormationCircular cylinder, Re = 100000, M ~ 0Large Eddy SimulationInstitute of Computational Fluid DynamicsJapan
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3b Viscous Flow
Turbulence:
Laminar Flow:
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Re=3500, Turbulent boundary layerGuezenec and NagibIllinois Institute of Technology
Turbulence
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3c. Compressibility
• Incompressible Regime –
• Subsonic Regime –
• Transonic Regime –
• Supersonic Regime –
Importance of compressibility effects governed bycVM
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Flow Past a Circular Cylinder
Re = 10,000 and Mach approximately zero
Re = 110,000 and Mach = 0.45 Re = 1.35 M and Mach = 0.64
Pictures are from “An Album of Fluid Motion” by Van Dyke
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Flow Past a Circular Cylinder
Mach = 0.80 Mach = 0.90 Mach = 0.95 Mach = 0.98
Pictures are from “An Album of Fluid Motion” by Van Dyke
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Flow Past a Sphere
Mach = 1.53 Mach = 4.01
Pictures are from “An Album of Fluid Motion” by Van Dyke
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3c. CompressibilitySome Qualitative Effects
Hypersonic vehicle re-entryNASA Image Library
Shock wave:
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3c. Compressibility
• Expansion or isentropic compression wave:
Some Qualitative Effects
Cone-cylinder in supersonic free flight, Mach = 1.84.Picture from “An Album of Fluid Motion” by Van Dyke.
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Summary• What a fluid is. Its properties. The governing
laws• Reynolds number. Mach number• How Newton’s 2nd Law works as a vector
equation• Viscous effects: no-slip condition, boundary
layer, separation, wake, turbulence, laminar• Compressibility effects: Regimes, shock waves,
isentropic waves.• Initial ideas of concepts such as
streamlines/separation• Qualitative understanding