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8/8/2019 Newtonian derivation of Hubble's constant
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Newtonian derivation of Hubble's error (constant)
Greeting: I am Joe Nahhas founder of real time physics and astronomy
Modern sciences are based on time travel and time travel is not any science. I am not saying that
modern and Nobel scientists are Darwin's apes to say the least but what I am saying is that
modern and Nobel scientists are Alfred Nobel dumb apes to be exact and I dare Nobel
Hubble's law is V = H0 D and Hubble's constant is H0
Where V is recessional velocity of expanding Universe and D is the distance of a distant galaxy and
H0 = 74.2 km/sec/mega parsec (Adam Reiss 2011 Nobel Prize winner)
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Abstract: Edwin's Hubble law/constant is 350 years error made by Newton's law wrong
solution and Leonhard Euler wrong mathematics and Henry Cavendish wrong experiments
and silly Einstein thought ideas and adopted by Alfred Nobel Mafia for prizes and fame and
dumb apes Nobel science. Astronomers give the value ofH0 = 74.2 kilometers per second per
million parsec. Astronomers give Sun - Earth distance x149 598, 000,000meters
1 parsec = [360x60x60/2 ] x149 598, 000,000 = 3.085680248x 1016 metersThe speed of light = 299 792 458 m / s; Earth's radius is re = 6371000 meters
Earth's spin period Te = 86164.1 seconds; clock's period Ts = 24 hours = 86400 seconds
H0 = 74.2 km/sec/ mega parsec is the rate of the expansion of the Universe!
1- Earth Rotate and usingTs= 24 hours = 86400 seconds instead of Te= 86164
Seconds will produce a visual illusion of(Te/ Ts)
2 - Earth rotate and observer not located at the center of Earth will be tracing the
circumference of earth disc (2 re)
3 - Earth rotate and astronomers gives light a velocity of c = 299792458 meter/second?
The problem with light velocity is the following:
A - Two objects going in the same direction each with velocity of 299792458 meters/ second and
their relative velocity is 299792458 meters/second
--------------------------------------------->>>>>>>>>>>>>>>>>>>>--------------------
--------------------------------------------->>>>>>>>>>>>>>>>>>>---------------------
B - Two objects going in the opposite directions each with velocity of 299792458 meters/ second
and their relative velocity is 299792458 meters/second
-------------------------------------------->>>>>>>>>>>>>>>>>>>>>>---------------------
----------
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I- light vertical Visualization angle 23.44
A disc on a rotating spherical Earth has a circumferenceof 2 re and 2 re / re = 2 .
Modern Nobel physicists and astronomers measurements were/are made in an inverse
square distance Newton's law and that would make the error 1/ (2). Modern Nobel
physicists and astronomers measure space distance vertically and that would make thevertical error Sine-1[1/ (2)]. Modern Nobel physicists and astronomers use standard
time period Ts = 24 hours = 86400 seconds and not Earth's spin period Te = 86164
seconds and that bring the measurement error to (Te/ Ts) Sine-1[1/ (2)]. Modern
Nobel physicists and astronomers measure in air and not vacuum with air index of
refraction n a = 1.000293 brings the total measurement error to a value equals to:
Error 1is the celestial sphere:(1/ n a) (Te/ Ts) Sine-1[1/ (2)] = 23.44
This celestial sphere is a visual illusion or measurement error of spherical Earth
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II - Light visualization constant c = 299792458 m/sec and not constant light velocity
Along the line of sight the measurement error is 2/ cosine 23.44 = 2 cosecant 23.44
In an Inverse square Newton's lawthe error is (2/ cosine 23.44) (2/ cosine 23.44)
= 4 2 / (cosine 23.44) 2
Light coming from stationary planets to stationary Earth and a rotating with Earth observer
with rotating Earth's radius will measure a time independent velocity error of
[4 2 re / (cosine 23.44) 2](1/t; t=1)
Using stand time Ts =86400 seconds and not Earth time Te = 86164 seconds and measuring in
air and not in vacuum makes the error amounts to:
[4 2 re / (cosine 23.44) 2] (1/t; t=1) (Ts/Te) 2 na2]
Astronomer's adjustment of time or multiplication by (Te/Ts) reduces the error to
Light visualization constantc = [42 (re/t)n2a /cosine2 23.44] (Ts/Te)
= 299792458 km/sec;re = 6,371,000 meters
The angle23.44 = cosine-1[2 n a (Te/Ts) (re/ct)]; t = 1 second
Celestial sphere error 2: 23.44 = cosine-1[2 n a (Te/Ts) (re/ct)]; t = 1sec
c = [42 (re/t)n2a /cosine2 23.44] (Ts/Te) = 299792458 km/sec; t = 1 sec
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II- Earth's Spin Visual velocities
a- Visual speed around the Sun
Distance r in a rotating sphere traces a circular distance 2 re
Angular velocity ' in a rotating sphere traces a circular 2 ' e
And Spin visual velocity is Vy= (2 r) (2 ' e) = 4 2 (' e re)
Vy= (2 r) (2 ' e) = 4 2 (' e re) = 4 2 (2 re / Te) = 18.34 km/sec
Measurements are based on standard Earth time Ts = 24 hours = 86400 seconds and not
Earth's actual time Te = 86164 seconds; (2 re / Te) = 0.464581 km/sec
In an Inverse square Newton's law the time error is: (Te/Ts) 2
Measurements are made in air: Dry air index of refraction 1.000274 - 1.000279
In an Inverse square Newton's law the Index of refraction error is: (1/n a2)
{[4 2 (2 re / Te)]/ [1 - Sine 23.44] (Te/Ts) 2- (2 re / Te)} (1/n a2) = 29.8 km/sec
18.34 km/sec + 29.8 km/sec = 48.14 km/sec
18.34 km/sec-29.8 km/sec = - 11.46 km/sec
18.34 km/sec - 11.46 km/sec = 6.88 km/sec
11.46 km/sec + 29.8 km/sec =41.26 km/sec
41.26 km/sec - (6.88 - 464581) [(n a Te/Ts)] 5= 35.1 km/sec
41.26 km/sec - (6.88 - 464581) = 34.844581
29.8 km/sec Earth w.r.to Sun motion Illusion
48.14 km/sec Mercury w.r.to Sun motion Illusion
35.1 km/sec Venus w.r.to Sun motion Illusion
48.14 km/secMercury w.r.to Earth Spin motion Illusion
41.26 km/sec Venus w.r.to Earth Spin motion Illusion
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III - Newton's equation is solved wrong for 350 years and the
correct solution deletes 112 of Nobel science and scientists:
F = -G m M/r2; r > 0
Physics Faculty wrong solution of ellipse, r (, 0) = a (1 - 2)/ (1 + cosine )
Correct solution is a rotating ellipse, r (, t) = [a (1-)/ (1+ cosine )] ( + ) t
Newton's equation in polar coordinates
F = m; = [r" - r '] r1+ [2 r' ' + r "] 1
With m (r" - r ')= - Gm M/r2 Eq-1
And 2 r' ' + r "= 0 Eq-2
I - Real numbers or time independent solution
Eq-2: 2 r' ' + r "= 0
Multiply by r> 0
Then 2 r r' ' + r2"= 0
Or, d (r')/d t = 0
And integrating: r' = h = constant
With m (r" - r ')= - Gm M/r2
Then, (r" - r ')= - GM/r2
Let u = 1/r; r = 1/u; r' = h = /u
And r' = d r/d t = (d r/ d u) (d u /d ) (d / d t)
= (- /u ) (d u /d ) '
= (-'/u ) (d u /d )
= - h (d u/ d )
And r' = d r/d t = - h (d u/ d )
And r" = d r/ d t = d (d r'/ d t)/ d t
= d [- h (d u/ d )]/ d t
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Multiply (d / d )
Then r" = d r/ d t = {d [- h (d u/ d )]/ d t} (d / d )
= ' {d [- h (d u/ d )]/ d }
= - h (d u/ d )
= (- h/r) (d u/ d )
= - h u (d u/ d )
And r" = d r/ d t = - h u (d u/ d )
With d r/dt - r ' = - G M/r2 E q 1
And - h u (d u/ d ) (1/u) (h u) = - G M u2
Then (d u/ d ) + u = G M/h2
And u = G M/h2+ A cosine
The r = 1/u = 1/ (G M/h2+ A cosine ); divide by G M/h2
And r = (h2/G M)/ [1 + (A h2/G M) cosine ]
With; h2/G M = a (1 - 2); (A h2/G M) =
This is Newton's equation classical solution
Or, r = a (1 - 2)/ (1 + cosine ); definition of an ellipse ------------- I
Newton's time independent solution
II - Real time or complex numbers solution :
Newton's equation in polar coordinates
F = m; = [r" - r '] r1+ [2 r' ' + r "] 1
With m (r" - r ')= - Gm M/r2 Eq-1
And 2 r' ' + r "= 0 Eq-2
Eq-2: 2 r' ' + r "= 0
Separate the variables: 2 r' ' = - r "
Or 2(r'/r) = - ("/') = - 2 ( + )
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Then: (r'/r) = +
Or d r/r = ( + ) d t
Then r = r 0(+ )t
And r = r (, 0) r (0, t); r 0= r (, 0)
And r = r (, 0) (+ )t
And r (0, t) = (+ )t
With r (, 0) = a (1 - 2)/ (1 + cosine )
Then, r (, t) = [a (1-)/ (1+ cosine )] (+ )t ------------- I
Newton's time dependent solution = quantum mechanics
If time is frozen that is t = 0
Then r (, 0) = a (1-)/ (1+ cosine ) or classical
Relativistic is the difference between I and Real II
With - ("/') = - 2 ( + )
Then ' = '0 -2 (+ )t
With '0 = h/[r (, 0)] 2
And '(, t) = [' (, 0)] -2(+ )t
And, '(, t) = ' (, 0) ' (0, t)
And ' (0, t) = -2(+ )t
At Perihelion:
We Have ' (0, 0) = h (0, 0)/r (0, 0) = 2ab/ 0 a (1- ) ;0 = orbital period
= 2a [ (1- )]/0a (1- ) ]
= 2[ (1- )]/0 (1- ) ]
Then '(0, t) = 2 [(1- )/ 0 (1- ) ] -2(+ )t
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With = 0
Then '(0, t) = 2 [(1-)/ 0 (1-) ] -2(+ )t
= 2 [(1-)/ 0 (1- ) ] (cosine 2 t - sine 2 t)
Real '(0, t) = 2 [(1- )/ 0 (1-) ] cosine 2 t
Real '(0, t) = 2 [(1-)/ 0 (1-) ] (1 - 2sine t)
Naming ' = '(0, t); '0 = 2 [(1-)/ 0 (1-) ]
Then ' = 2 [(1- )/ 0 (1- ) ] (1 - 2 sine t)
And ' = '0 (1 - 2 sine t)
And ' - '0 = - 2 '0 sine t = -2{2 [(1-)/ 0 (1-) ]} sine tAnd ' - '0 = -4 [(1-)/0 (1-) ] sine t
With, v = spin velocity; v0 = orbital velocity; 0 = orbital period
And 0= tan-1 [(v + v0)/c]; light aberrations
' = ' - '0
= - 4 [(1-)]/0 (1-) ] sine tan-1 [(v + v0)/c] radians per0
In degrees per period is multiplication by 180/
' = (-720) [(1-)/0 (1-) ] sine tan-1 [(v + v0)/c]
The angle difference in degrees per period is: = ( ') 0
= (-720) [(1-)/(1-) ] sine tan-1 [(v + v0)/c] calculated in degrees per century is
multiplication = 100 ;= Earth orbital period = 100 x 365.26 =36526 days and dividing byusing 0 in days: (100 /0)= in degrees per century
= (-72000 /0) [(1-)/ (1-) ] sine tan-1 [(v + v0)/c]
In arc second per century is multiplying by 3600
= - 3600 x 720 (100 /0) [(1-)/ (1-) ] x Sine tan-1 [(v + v0)/c]
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Approximations I
With v
8/8/2019 Newtonian derivation of Hubble's constant
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Or, r = a (1 - 2)/ (1 + cosine ); definition of an ellipse
Rotating ellipse, r (, t) = [a (1-)/ (1+ cosine )] (+ )t ------------- I
Equation I quantum Mechanics and Equation II is classical mechanics
G has a unit dimension [1/density, 1/time 2] = [1/air density, 1/ Earth period 2] = [a, Te2]
Earth's spherical dry air density is 1.2041The measurement of G using spring method which
involves moment of inertia or summations introduces (2/5) error and around a sphere introduces
(4/3). Measuring in air introduces air index of refraction error n a
G = 1/ (4/3) (2/5) a Te2
n a=6.674 x 10
-11
; a =1. 2041 kg/ m3
; n a2
=1.000293
Earth's orbital period is Te = 86164 second; Earth's time period = 24 hours = 86400 seconds
Dry air density is 1.2041 kg/ m3; air index of refraction at 1.000293
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Classical says: Index of refraction is an embedded error n a
And using an inverse square law of Isaac Newton introduces (Ts/Te) 2 error
Quantum founded by Plank introduces a 5th power factor from Plank's law of black body
radiation and the embedded error is 1/n a5
The total error (1/n a) 5 (Ts/Te) 2
The fine structure constant = 1/137.03599 is a measurement error
This quantum error comes from Boltzmann
(1/n a) 5 (Ts/Te) 2 Cosine -1 [1/Ln-1] =23.44
Almost everything humans know about Physical sciences including physics astronomy physical
chemistry and physical biology is all wrong because humans measure/measured wrong since the
beginning of time and Earth's spin and Earth's spherical shape and Earth's air density and air
index of refraction and Earth's spin periods introduces errors called modern Nobel science
Plank h = 6.62606957 x 10- 34joule -second is an error.
IV Plankassumed light velocity c =299792458 km/sec and ended up giving planet Earth a light
Velocity c = 299792458 km/sec
Earth's radius re = 637100 meters/second; Earth's density = 5515 kilogram
Earth's mass me= (4 /3) re3=5.973886146 x 10 24kilogram
Light - Earth's momentumme c = 1.790926012 x 1033kilogram meter/second
The division (1/ me c)/h = 0.842687136 and in an Inverse square law the (0.842687136) =
0.917979921 and 0.91799921/ n a2= 0.91799921/1.0002782 (dry air index of refraction)
= cosine 23.44
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1 - Real time distance
1 = 1 is self evident; 2 = 2 is self evident
A = A is self evident; B = B is self evident
Or B = B; add and subtract A
A = B + (B - A); divide by A
(A/B) = 1 + (A - B)/B; multiply by D
(A/B) D = D + [(A - B)/B] D --------------------------------- Equation - 1
C = C is self evident; D = D is self evident
Or C = C; add and subtract D
C = D + (C - D) ----------------------------------------------- Equation - 2
Comparing equations 1 and 2 yields, (1) AC = BD; (2) D = D; and (3)
C - D = [(A - B)/B] D
Or (C - D)/D = (A - B)/B
Or D/D = B/B; Divide by t
(1/D) ( D/ t) = (1/B) ( B/ t)
Limit [(1/D) ( D/ t)] = Limit [(1/B) ( B/ t)] = ( + )
t --- 0 t --- 0
Or, d B/B = ( + ) d t
Or, B = B0 e ( + ) t = Ae ( + ) t
B = Ae ( + ) t
Distance is A; real time distance is B = Ae ( + ) t
Or in general real time distance is r = r0 e ( + ) t
2 - Real time velocity
With r = r0 e ( + ) t; real time velocity is v = [v0 + ( + ) r0] e ( + ) t
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Edwin Hubble: A professional astronomer at Macdonald
Nobel Institution is where Alfred Nobel honors the most dangerous criminals
Cavendish experimental error of5/2: G = 1/ (4/3) (2/5) a Te2 n a
Celestial sphere error: (2):(1/ n a) (Te/ Ts) Sine-1[1/ (2)] = 23.44
5/2 (2); 2/5 1/ (2); 2/5 [1/ (2)] (Te/ Ts)
With ' = '0 -2 ( + ) t
Or, ' = '0 -2 t + 2 t
And ' = ' x+ ' y= '0 -2 t [cosine 2 t + cosine 2 t]
Along the line of sight ' x= '0 -2 t cosine 2 t
And ' x= '0 -2 t [1- 2 sine 2 t]
With ' x = 2/T; '0 = 2/T0
[(2/T) - (2/T0)] = - (4/T0) -2 t sine 2 t
With -2 t= (2 ); wt = arc tan (v/c)
[(2/T) - (2/T0)] = (4/T0) (2 ) sine 2 arc tan (v/c)
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Hubble's constant H0 = 74.2 km/second per mega parsec
1 parsec = [360x60x60/2 ] x149 598, 000,0001 mega parsec = [360x60x60/2 ] x149 598, 000,000 x 1,000,000
74.2 km/sec per mega parsec
H0= 74,200 / {[360x60x60/2 ] x149 598, 000,000 x 1,000,000} = 2.4 x 10-18 sec-1
H0= (4/T0) (2 ) sine 2 arc tan (v/c)
T0 = Earth orbital period 365.251 days; v = Earth's spin velocity = 464.581 m/sec; c= light
velocity = 299792458 m/sec
H0 = [(2/T) - (2/T0)] = (4/T0) (2 ) sine 2 arc tan (v/c)
= (4/365.251 x 86164.0989) (2 ) sine 2 arc tan (464.581/299792458)
(4/365.251) (2 )(464.581/299792458)2 = 2.4 x 10-18
= 74.2 km/sec/mega parsec
Conclusion: Edwin Hubble made the following errors
1- Real time measurements r = r0 e ( + ) t; ' = '0 -2 ( + ) t
2- Spherical error (2 )
3- Measured = H0 = [(2/T) - (2/T0)] (2 )(4/T0) (v/c) 2
Edwin Hubble was/is a professional astronomer at Macdonald's or NASA
because there is no difference between NASA and Macdonald's of a big bang
that no one heard and dark energy that no one can find and time travel that
no one can perform!!!!!!!!!!!!!!!Etc
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