- •Give the definition of the stream line, write its differential equation.
- •Give the definition of the stream surface, infinitesimal stream tube.
- •Essence of Eulers method for investigation of fluid motion .
- •Essence of Lagrange method for investigation of fluid motion .
- •Accordance between path line, streamline, Eulers and Lagrange methods for investigation of fluid motion
- •What is the base for obtaining continuity equation?
- •Write 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 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?
- •Write differential form of continuity equation for steady flow and call its members.
- •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?
Write the gas state equation and call its members.
Where P – pressure
R
- gas constant (for air R=287
)
– density
T – temperature
Give the definition of the gas compressibility; which index is used in order to characterize compressibility.
Gas Compressibility (cg)
The compressibility of a substance is the change in volume per unit volume per unit change in pressure. The gas compressibility should not be confused with the compressibility factor (z), which is the deviation factor from ideal gas behavior. The gas compressibility is calculated from the BWR equation of state as published in the ERCB manual "Gas Well Testing - Theory and Practice".
The gas compressibility is a very strong function of pressure and increases as the pressure decreases. Mathematically, it can be expressed as:
Where p is the specified pressure and z is the gas compressibility factor (z) at that pressure. Thus, the magnitude of gas compressibility (cg) is of the order of 1 / p. Moreover, when the pressure drawdown at the wellbore is large, the difference in compressibility values at the initial pressure (pi) and at the flowing pressure is significant and must be accounted for by using the pseudo-time (ta) variable, instead of regular time.
Gas Compressibility Factor (z)
The compressibility factor of a natural gas is a measure of its deviation from ideal gas behavior. Its value is usually between 0.8 and 1.2, but it can be as low as 0.3 and as high as 2.0. It is used in the calculation of gas pseudo-pressures (y), and in converting gas volumes and rates from standard conditions to reservoir conditions (and vice-versa). It is sometimes called the super-compressibility factor, and is often confused with the term "compressibility" (which is the change in volume per unit volume per unit change in pressure). The gas compressibility factor directly affects the gas compressibility (cg).
Give the definition of the gas viscosity; which index is used in order to characterize viscosity.
The viscosity of a fluid is a measure of its resistance to gradual deformation by shear stress or tensile stress. Viscosity is due to friction between neighboring parcels of the fluid that are moving at different velocities. When fluid is forced through a tube, the fluid generally moves faster near the axis and very little near the walls, therefore some stress (such as a pressure difference between the two ends of the tube) is needed to overcome the friction between layers and keep the fluid moving. For the same velocity pattern, the stress is proportional to the fluid's viscosity.
A fluid that has no resistance to shear stress is known as an ideal fluid or inviscid fluid. In the real world, zero viscosity is observed only atvery low temperatures, in superfluids. Otherwise all fluids have positive viscosity. If the viscosity is very high, such as in pitch, the fluid will seem to be a solid in the short term. In common usage, a liquid whose viscosity is less than that of water is known as a mobile liquid, while a substance with a viscosity substantially greater than water is simply called a viscous liquid.
Viscosity is a measure of the degree momentum transport in a fluid perpendicular to flow velocity due to flow shear. The momentum is ultimately carried by the individual molecules. A gas is defined as a fluid in which the molecules are more or less free, except for discrete scattering events with other molecules. Unless the gas is ionized, the collision cross section varies little with impact velocity. Therefore, as the temperature (free velocity) increases, the molecules carry more momentum and collide more often. That means more viscous momentum transport.
Viscosity in gases arises principally from the molecular diffusion that transports momentum between layers of flow. The kinetic theory of gases allows accurate prediction of the behavior of gaseous viscosity.
