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

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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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