- Resistance type nozzle - Diffuser (surface angle change < 80 )
Resistors in series
ΣU = 0, Uimput + UF + Uoutput = 0, (U vector, ρ = const.)
Is = constant A1 us1 = A2 us2, us2 = us1 A1 / A2 (us = supply velocity)
The form voltage (because of surface flow change)
ΔU = UF = (ΔR) I + (ΔΙ) R = (R1 - R2)I = RF I
the form resistance RF (flow surface A1 to surface A2)
RF = R1 - R2 = (u1 / ρ A1) - (u2 / ρ A2), I = ρA1 u1 →
UF = RF I = u12 - u1 u2 A1 / A2 = U1 - U2 = u12- u22 →
→ u22 = u1 u2 A1 / A2 → u1 A1 = u2 A2
Potential velocity change at nozzle is proportionate to surface
UF = u12{1 - [A1 / A2] 2} is negative at nozzle, positive at Diffuser (in analogy to PTC- thermistor).
RF = γ R1, γ = 1 - [A1 / A2]2
The form voltage is maintained in the system and can be used in propulsion systems such as common Spoiler or nozzle drive (Laval ). For supersonic transition velocity the calculation includes also thermal voltage (change of charge density ρ).
- Hydroelectric Station (flow intensity – supply)
Water with flow supply I = Q/t = 103 Kg/sec initiate a turbine (LT Power Turbine shaft). The diameter of water pipe surface A is constant. The input pressure on entrance is P1 = 500 KPa, on exit P5 = 123 KPa and the elevation difference is r = 10,5 m . Friction losses amount to L r = 80 KJ / sec. Density of water ρ = 1000 Kg / m3, thermal coefficient of water c = Lr / I ΔΤ = 4,18 KJ / Kg K. Earth's gravitational field density g = 9,81 V / m.
Requisites: power turbine shaft LT, temperature variation ΔΤ, efficiency factor n, capacity C, internal resistance R, conductor diameter d.
1. Input Voltage (+). 2. Elevation Voltage (+). 3. Friction voltage drop (-). 4. Turbine voltage drop (-) 5. Output Voltage (-).
U1 = P1 / ρ, U2 = g r, U3 = L r / I = c ΔT, U4 = LT / I, U5 = P5 / ρ
ΣU = 0, U4 = U1 + U2 - U3 - U5 = 400V,
Capacity C = Q/(U1 + U2) = t 10 3 Kg, by 603 V (min. for t = 10 years, otherwise the investment is not amortized!).
Internal resistance Ri = R3 = U3 / I = 0,08 {Ω}
Pipe diameter: P1 = ρ u12 → dynamic velocity u1 = 22,36 m/sec and pipeline diameter from A1 = πd 2 / 4 = L1/ρ u13, (L1 = U1I) → d = 0,2386 m
This example clarifies the relationship potential - flow Intensity / supply, the role of dynamic velocity (u5 = 11,09 m/sec) and the role of the pipe surface A as necessary resistance (equivalent to an electrical).
At the exit (if the ambient pressure = 101.325 Pa) dynamic velocity could be reduced to u5= 10,07 m/s, corresponding to 21,7 Kw of extra turbine power.
The kinetic energy (transition velocity us1) is unable to express voltage. The transition velocity (supply) is at the exit also us1 = us5 = 22,36 m/sec (A1 us1 = A5 us5 ) but: A1 u1 ≠ A5 u5) where A = constant.
- Attempt to calculate the mass density limits
3.1 The minimum pressure P is equal to the measure of the gravitational constant G (P = G).
3.2 Cosmic Potential U has the maximum value (U max = c2 / 2 ) of a sphere
3.3 Energy has one form.
Since the potential (within the limits of the system) is maintained, the minimum pressure rise to the minimum charge density equal to:
ρ min = P / U = 2G / c2
Equation (8) shows the maximum radius to:
r max = (3 / π) 1/2 c2 / 4G
i.e. the total mass equivalent:
Σm = (3 / π)1/2 c4 / 8G2 = 2,222 1055 Kg
In this case (no necessary dark energy) the amount of energy was in the shape of area E = PV, not stars.
3.4 By maximum charge density the dynamic velocity provides maximum angular velocity ω = 2π, so that it can not add another one mass because potential is at the maximum U = c2 / 2 (at the surface of the sphere, the intensity of gravity is g = c2 π21/2).
At maximum concentration from the equation u = ω r = 2πr, is given:
sphere radius r = c / π 81/ 2
maximum charge density ρ max = 3π / G
but the mass obtained for maximum capacity is equal to:
m = c3 /2πG 81/2 = 2, 28 1034
corresponding to a space Vm = c5 /4πG2 81/2 charge density of ρ = 2G / c2
This precluded the gathering of all energy in the form of a mass, but in 1021 spaces Vm, which are due to their potential in alternating voltage (Universe can not be in a single energy form).
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