
- •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?
Write differential form of continuity equation for steady flow and call its members.
The continuity equation states that, in any steady state process, the rate at which mass enters a system is equal to the rate at which mass leaves the system.
The differential form of the continuity equation is:
where
ρ is fluid density,
t is time,
u is the flow velocity vector field.
In this context, this equation is also one of Euler equations. The Navier-Stokes equations form a vector continuity equation describing the conservation of linear momentum.
Steady
flow
Write differential form of continuity equation for incompressible flow and call its members.
The differential form of the continuity equation is:[1]
where
ρ is fluid density,
t is time,
u is the flow velocity vector field If ρ is a constant, as in the case of incompressible flow, the mass continuity equation simplifies to a volume continuity equation:[1]
which means that the divergence of velocity field is zero everywhere. Physically, this is equivalent to saying that the local volume dilation rate is zero.
W rite continuity equation for infinitesimal stream tube, one dimensional flow with finite cross section area and call its members.
Where A – is a cross-section area
This equation is general continuity equation for one dimensional flow.
Which physical values are considered as gas state parameters?
Parameter 1: Temperature
Temperature (T) is an indicator of the average kinetic energy that a sample of matter possesses. If a sample could be viewed nanoscopically (on a scale of 10-9 meters), its constituent particles would be observed to be in constant motion. The nature of these motions would become increasingly disordered as the state of matter varies- solids would undergo a more harmonic, organized motion, gases a completely chaotic motion, and liquids somewhere in between. A "hot" body would be observed to have more of this kinetic motion than a "cooler" body. If two systems are able to exchange energy of motion (a condition called thermal contact), a faster-moving body would naturally transfer momentum to a slower-moving body. The rate and magnitude of this transfer depends on the bonding relationships which macroscopically act as the heat capacity of matter, allowing some materials to heat or cool more dramatically than others. Energy continues to flow from hot to cold until the two bodies reach thermal equilibrium, where momentum is equally transferred between the two. The bodies are then said to be at the same temperature. To assign temperature, we place a body in thermal contact and allow it to come to thermal equilibrium with a device called a thermometer. Traditionally a liquid (typically mercury or alcohol) with known coefficient of expansion is used as a thermometer. Heating expands and cooling contracts the liquid, and these processes can be calibrated to one of the accepted temperature scales. A digital thermometer passes a fixed current through a metal probe. The probe has a temperature-dependent change in resistance, so resulting output voltage accurately measures the temperature of a system.
Parameter 2: Pressure
Pressure (the symbol: p) is the ratio of force to the area over which that force is distributed.
Pressure is force per unit area applied in a direction perpendicular to the surface of an object. Gauge pressure (also spelled gage pressure)[a] is the pressure relative to the local atmospheric or ambient pressure. While pressure may be measured in any unit of force divided by any unit of area, the SI unit of pressure (the newton per square metre) is called the pascal (Pa) after the seventeenth-century philosopher and scientist Blaise Pascal. A pressure of 1 Pa is small; it approximately equals the pressure exerted by a dollar bill resting flat on a table. Everyday pressures are often stated in kilopascals (1 kPa = 1000 Pa).
Fluid pressure is the pressure at some point within a fluid, such as water or air (for more information specifically about liquid pressure, see section below).
Fluid pressure occurs in one of two situations:
an open condition, called "open channel flow"
the ocean, or
swimming pool, or
the atmosphere.
a closed condition, called closed conduits
water line, or
gas line.
Parameter 3: Density
The density of air, ρ (Greek: rho) (air density), is the mass per unit volume of Earth's atmosphere, and is a useful value in aeronautics and other sciences. Air density decreases with increasing altitude, as does air pressure. It also changes with variances in temperature or humidity. At sea level and at 15 °C according to ISA (International Standard Atmosphere), air has a density of approximately 1.225 kg/m3 (0.0023769 slugs/ft3).