
- •What is the base for obtaining continuity equation?
- •69Write integral form of continuity equation and call its members.
- •Write differential form of continuity equation and call its members.
- •Write differential form of continuity equation for steady flow and call its members.
- •Write differential form of continuity equation for incompressible flow and call its members.
- •W rite continuity equation for infinitesimal stream tube, one dimensional flow with finite cross section area and call its members.
- •Which physical values are considered as gas state parameters?
- •Temperature and pressure
- •Write the gas state equation and call its members.
- •Give the definition of the gas compressibility; which index is used in order to characterize compressibility.
- •Give the definition of the gas viscosity; which index is used in order to characterize viscosity.
- •Write the Newton’s formula for internal friction and call its members.
- •Write formula for calculation Reynolds number (Re). Call its members.
- •Write the formula for calculation the speed of sound using gas temperature; and call its members.
- •How (quality) does change dynamic coefficient of viscosity when temperature of gas changes? The same for liquid.
- •Call physical values whose fields completely describe the phenomenon of flow around the solid body.
- •Which type of thermodynamic process in aerodynamics usually is used ? Call this thermodynamic process, write its formula, call members of this formula.
- •Write formulas for calculation gas parameter relation in flow stagnation point and free stream condition. Call members of these formulas.
- •Give the definition the critical or sonic flow regime.
- •What is critical speed of sound?
- •Write formula for calculation theoretical maximum speed of flow and call its members.
- •What is the velocity factor? What is difference between the velocity factor and Mach number?
- •Write formula for calculation flight Mach number using instrumental measured pressure values.
- •Call the conformity between flight regimes and Mach number values. Subsonic and Supersonic speed
- •Write Gugonio equation, call its members.
- •Name and give definitions of two viscosity flow regimes.
- •Give the definition of the boundary layer.
- •Draw schemes of viscose air flow about solid body surface. Mark main elements of this flow.
- •Relation between which forces does Reynolds number (Re) characterize? Write the formula for Reynolds number calculation, call physical values used in this formula.
- •Relation between which forces does Fruds number (Fr) characterize? Write the formula for Fruds number calculation, call physical values used in this formula.
- •Relation between which forces does Eulers (Eu) number characterize? Write the formula for Eulers number calculation, call physical values used in this formula.
- •Relation between which forces does Mach number (m) characterize? Write the formula for Mach number calculation, call physical values used in this formula.
- •Relation between which forces does Struhal number (St) characterize? Write the formula for Struhal number calculation, call physical values used in this formula.
- •Relation between which forces does turbulance degree (ε) characterize?
What is the base for obtaining continuity equation?
One of the fundamental principles used in the analysis of uniform flow is known as the Continuity of Flow. This principle is derived from the fact that mass is always conserved in fluid systems regardless of the pipeline complexity or direction of flow. When a fluid is in motion, it must move in such a way that mass is conserved. To see how mass conservation places restrictions on the velocity field, consider the steady flow of fluid through a duct (that is, the inlet and outlet flows do not vary with time). The inflow and outflow are one-dimensional, so that the velocity V and density \rho are constant over the area A (figure 14).
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Figure 14. One-dimensional duct showing control volume. |
Now we apply the principle of mass conservation. Since there is no flow through the side walls of the duct, what mass comes in over A_1 goes out of A_2, (the flow is steady so that there is no mass accumulation). Over a short time interval \Delta t,
Or
Where:
Q = the volumetric flow rate
A = the cross sectional area of flow
V = the mean velocity
This is a statement of the principle of mass conservation for a steady, one-dimensional flow, with one inlet and one outlet. This equation is called the continuity equation for steady one-dimensional flow. For a steady flow through a control volume with many inlets and outlets, the net mass flow must be zero, where inflows are negative and outflows are positive.
69Write integral form of continuity equation and call its members.
or
where
S is a surface as described above - except this time it has to be a closed surface that encloses a volume V,
denotes
a surface
integral over
a closed surface,
denotes
a volume
integral over V.
is
the total amount of ρ in
the volume V;
is
the total generation (negative in the case of removal) per unit time
by the sources and sinks in the volume V,
Write differential form of continuity equation and call its members.
The differential form for a general continuity equation is (using the same q, ρ and j as above):
Where
∇• is divergence,
t is time,
σ is the generation of q per unit volume per unit time. Terms that generate (σ > 0) or remove (σ < 0) q are referred to as a "sources" and "sinks" respectively.
This general equation may be used to derive any continuity equation, ranging from as simple as the volume continuity equation to as complicated as the Navier–Stokes equations. This equation also generalizes the advection equation. Other equations in physics, such as Gauss's law of the electric field and Gauss's law for gravity, have a similar mathematical form to the continuity equation, but are not usually called by the term "continuity equation", because j in those cases does not represent the flow of a real physical quantity.
In the case that q is a conserved quantity that cannot be created or destroyed (such as energy), this translates to σ = 0, and the continuity equation is: