Ryuu Blog

if you find an 1/8 marathons count me in

dang *I should have said 1/16 *

!!

Hi, Heiko. Welcome back.

I have an experience participating a full course marathon in 2005, but the record was very bad. It was almost 5 hours.

Good luck to you.

hehe

...fat chance

Hallo~ Ich wuerde seit September in HS Esslingen studieren. In welcher Stadt wohnst du?

Viele Gruesse,
Antonia

I never knew there was an Einstein marathon. Keep training and you'll be the winner

That's a very good idea to start training early and regularly, I have never tried to run a marathon, it's not easy, I know, but good for you.

Spring is here, I am going to do regular hiking too... hope I can condition myself for a long hike in summer time...

Glad you are blogging again!

Ich studiere Mechatronik. Du kommst aber kaum zu diesem blog..

Vielen Dank! Heiko.
Ich glaube,dass ich gut Zeit in Deutschland haben wuerde.
Warte auf deinen ausgezeichneten Blog~~

Und doch viele Gruesse in 2008:)

Yes, I hike in spring and fall too, in summer time I like to hike for long distance, sometimes go camping with friends in national parks, very beautiful!

祝你好心情！

P.S. Sorry for the late reply...

Great Design ! congrats

Man! Nice work!
I am amazed!
Probably the best web design I've ever seen!

May I peek around to see how was it done?

Congrats!

Anonymous writes: Kepler (demolish) Vs Einstein's space jail of time r -------------- Exp (i wt) -----------S= r Exp (ì wt) Nahhas' Equation Orbit location-----------Orbit light sensing -------------- Visual orbit location Particle/Newton ---------------- --Visual -------------------------- Wave/Quantum Quantum - Newton=visual effects=relativistic effects=space-time confusions S= visual distance; r = actual distance; v = speed and c = light speed S = r Exp (i wt) = r [cosine (wt) + î sine (wt)] P =d S/d t = v Exp (ì w t) + ì r w Exp (ì w t); v=d r/d t; v=w r = v (1+ ì) [Exp (ì wt)] = visual velocity E (definition) = m/2(m v + m' r) ²; E = mc²/2 If v = 0; m' r=mc E (visual) = mp²/2 = mv²/2(1+ì) ² Exp 2(ì w t) E (visual) = mv²/2(1 + 2ì -1) [cos2wt + ì sin2wt] E (visual) = ì (mv²) [1-2sin²wt + 2i [sin (wt)] [cosine (wt)] If wt = (2n+1) π/4 E (visual) = ì (mv²) [1-1 ± ỉ] = ± (mc²); v = c 2-Central force law Areal velocity is constant: r² (d θ/d t) =h Kepler's Law h = 2π a b/T; b=a√ (1-ε²); a = mean distance value; ε = eccentricity r² (d θ/d t) = h = S² (d w/d t) Replace r with S = r exp (ỉ wt); h = [r² Exp (2iwt)] (d w/d t) (d w/d t) = (h/r²) exp [-2(i wt)] d w/d t= (h/r²) [cosine 2(wt) - ỉ sine 2(wt)] = (h/r²) [1- 2sine² (wt) - ỉ sin 2(wt)] d w/d t = d w(x)/d t + d w(y)/d t; d w(x)/d t = (h/r²) [ 1- 2sine² (wt)] d w(x)/d t – (h/r²) = - 2(h/r²)sine²(wt) = - 2(h/r²)(v/c)² v/c=sine wt (h/ r²)(Perihelion/Periastron)= [2πa.a√ (1-ε²)]/Ta² (1-ε) ²= [2π√ (1-ε²)]/T (1-ε) ² Δ w/d t = (d w/d t – h/r²] = -4π {[√ (1-ε²)]/T (1-ε) ²} (v/c) ² radian per second Δ w/d t = (- 4π /T) {[√ (1-ε²)]/ (1-ε) ²} (v/c) ² radians Δ w°/d t = (-720/T) {[√ (1-ε²)]/ (1-ε) ²} (v/c) ² degrees; Multiplication by 180/π Δ w°/d t = (-720x36526/T) {[√ (1-ε²)]/(1-ε)²} (v/c)² degrees/100 years Δ w”/d t = (-720x3600/T) {[√ (1-ε²)]/(1-ε) ²} (v/c) ² seconds of arc multiplication by 3600 Δ w/d t = (-720x36526x3600/T) {[√ (1-ε²]/(1-ε)²} (v/c)² seconds of arc per century The circumference of an ellipse: 2πa (1 - ε²/4 + 3/16(ε²)²- --.) ≈ 2πa (1-ε²/4); R =a (1-ε²/4) v=√ [G m M / (m + M) a (1-ε²/4)] ≈ √ [GM/a (1-ε²/4)]; m<<M; Solar system Application 3: Advance of Perihelion of mercury. G=6.673x10^-11; M=2x10^30kg; m=.32x10^24kg ε = 0.206; T=88days; c = 299792.458 km/sec; a = 58.2km/sec Calculations yields: v =48.14km/sec [√ (1- ε²)] (1-ε) ² = 1.552 Δ w”= (-720x36526x3600/88) x (1.552) (48.14/299792)²=43.0”/century Conclusions: E ≠ mc² (special-relativity) and the 43" seconds of arc of advance of perihelion of Planet mercury (general-relativity) is are caused by deformed space-time physicists "thought" and not deformed space (x, y, z). Anyone dare to prove me wrong? E=mc²/2 E (Energy by definition) = mv²/2 = mc²/2; if v = c m = mass; v= speed; c= light speed; w= angular velocity; t= time S = r Exp (ì w t) = r [cos (wt) + ì sin (wt)] Visual effects P = visual velocity = change of visual location P = d S/d t = v Exp (ì w t) + ì w r Exp (ì w t) = (v + ì w r) Exp (ì w t) = v (1 + ì) Exp (ì w t) = visual speed; v = w r E (visual energy= what you see in lab) = m p²/2; replace v by p in E = mv²/2 = m p²/2 = m v²/2 (1 + ì) ² Exp (2ì wt) = mv²/2 (2ì) [cosine (2wt) + ì sine (2wt)] =ì mv² [1 - 2 sine² (wt) + 2 ì sine (wt) cosine (wt)];v = speed; c = light speed wt = π/2 E (visual) = ìmv² (1 - 2 + 0) E (visual) = -ì mc² ≡ mc² (absolute value;-ì = negative complex unit) If v = c w t = π/4 E (visual) = imv² [1-1 +ỉ] =-mc²; v = c wt =-π/4+ỉln2/2; 2ỉ wt=-ỉπ/2 - ln2 Exp (2i wt) = Exp [-ỉπ/2] Exp [ln(1/2)]=[-ỉ (1/2)] E (visual) = imv² (-ỉ/2) =1/2mc² v = c Conclusion: E = mc² is the visual Illusion of E = mc²/2 joenahhas1958@yahoo.com. All rights reserved. PS: In case of E=mc² claims to be rest energy claims then E=1/2m (m v + m' r) ² = (1/2m) (m' r) ²; v = 0 E = (1/2m) (mc) ²; m' r =mc E=mc²/2 Space-time to the sewer------------------------------------------>

Anonymous writes: There is One and Only One Mechanics: Universal Mechanics: Ending Einstein's space-jail of time in 2009 joenahhas1958@yahoo.com Introduction to Universal Mechanics: For 350 years Physicists Astronomers and Mathematicians missed Kepler's time dependent equation introduced here and transformed Newton's equation into a time dependent Newton' equation and together these two equations explain Quantum - Relativistic effects; it combines classical mechanics and quantum mechanics into one mechanics and explains "relativistic" effects as the difference between time dependent measurements and time independent measurements of moving objects. Time is not a structure like space to scientifically accept space-to imaginary time - back to space jumping continuum (x, y, z, it) regardless of what all 100,000 living space-time physicists and Astrophysicists have said about it because Physics is a business and not necessarily science or scientific and like every business Physics comes with fraud and fraud is "junk" experimentation and junk based "thought" experimentation that led to fraud physics E=mc². All there is in the Universe is objects of mass m moving in space (x, y, z) at a location r = r (x, y, z). The state of any object in the Universe can be expressed as the product S = m r; State = mass x location: P = d S/d t = m (d r/dt) + (dm/dt) r = Total moment = change of location + change of mass = m v + m' r; v = velocity = d r/d t; m' = mass change rate F = d P/d t = d²S/dt² = Total force = m(d²r/dt²) +2(dm/dt)(d r/d t) + (d²m/dt²)r = mγ + 2m'v +m"r; γ = acceleration; m'' = mass acceleration rate In polar coordinates system r = r r(1) ;v = r' r(1) + r θ' θ(1) ; γ = (r" - rθ'²)r(1) + (2r'θ' + rθ")θ(1) F = m[(r"-rθ'²)r(1) + (2r'θ' + rθ")θ(1)] + 2m'[r'r(1) + rθ'θ(1)] + (m"r) r(1) = [d²(mr)/dt² - (mr)θ'²]r(1) + (1/mr)[d(m²r²θ')/dt]θ(1) = [-GmM/r²]r(1) d²(mr)/dt² - (mr)θ'² = -GmM/r² Newton's Gravitational Equation (1) d(m²r²θ')/dt = 0 Central force law (2) (2) : d(m²r²θ')/d t = 0 <==> m²r²θ' = [m²(θ,0)φ²(0,t)][ r²(θ,0)ψ²(0,t)][θ'(θ, t)] = [m²(θ,t)][r²(θ,t)][θ'(θ,t)] = [m²(θ,0)][r²(θ,0)][θ'(θ,0)] = [m²(θ,0)]h(θ,0);h(θ,0)=[r²(θ,0)][θ'(θ,0)] = H (0, 0) = m² (0, 0) h (0, 0) = m² (0, 0) r² (0, 0) θ'(0, 0) m = m (θ, 0) φ (0, t) = m (θ, 0) Exp [λ (m) + ì ω (m)] t; Exp = Exponential φ (0, t) = Exp [ λ (m) + ỉ ω (m)]t r = r(θ,0) ψ(0, t) = r(θ,0) Exp [λ(r) + ì ω(r)]t ψ(0, t) = Exp [λ(r) + ỉ ω (r)]t θ'(θ, t) = {H(0, 0)/[m²(θ,0) r(θ,0)]}Exp{-2{[λ(m) + λ(r)]t + ì [ω(m) + ω(r)]t}} ------I Kepler's time dependent equation that Physicists Astrophysicists and Mathematicians missed for 350 years that is going to demolish Einstein's space-jail of time θ'(0,t) = θ'(0,0) Exp{-2{[λ(m) + λ(r)]t + ỉ[ω(m) + ω(r)]t}} (1): d² (m r)/dt² - (m r) θ'² = -GmM/r² = -Gm³M/m²r² d² (m r)/dt² - (m r) θ'² = -Gm³ (θ, 0) φ³ (0, t) M/ (m²r²) Let m r =1/u d (m r)/d t = -u'/u² = -(1/u²)(θ')d u/d θ = (- θ'/u²)d u/d θ = -H d u/d θ d²(m r)/dt² = -Hθ'd²u/dθ² = - Hu²[d²u/dθ²] -Hu² [d²u/dθ²] -(1/u)(Hu²)² = -Gm³(θ,0)φ³(0,t)Mu² [d²u/ dθ²] + u = Gm³(θ,0)φ³(0,t)M/H² t = 0; φ³ (0, 0) = 1 u = Gm³(θ,0)M/H² + Acosθ =Gm(θ,0)M(θ,0)/h²(θ,0) mr = 1/u = 1/[Gm(θ,0)M(θ,0)/h(θ,0) + Acosθ] = [h²/Gm(θ,0)M(θ,0)]/{1 + [Ah²/Gm(θ,0)M(θ,0)][cosθ]} = [h²/Gm(θ,0)M(θ,0)]/(1 + εcosθ) mr = [a(1-ε²)/(1+εcosθ)]m(θ,0) r(θ,0) = [a(1-ε²)/(1+εcosθ)] m r = m(θ, t) r(θ, t) = m(θ,0)φ(0,t)r(θ,0)ψ(0,t) r(θ,t) = [a(1-ε²)/(1+εcosθ)]{Exp[λ(r)+ω(r)]t} Newton's time dependent Equation --------II If λ (m) ≈ 0 fixed mass and λ(r) ≈ 0 fixed orbit; then θ'(0,t) = θ'(0,0) Exp{-2ì[ω(m) + ω(r)]t} r(θ, t) = r(θ,0) r(0,t) = [a(1-ε²)/(1+εcosθ)] Exp m = m(θ,0) Exp = m(0,0) Exp [ỉ ω(m) t] ; m(0,0) θ'(0,t) = θ'(0, 0) Exp {-2ì[ω(m) + ω(r)]t} θ'(0,0)=h(0,0)/r²(0,0)=2πab/Ta²(1-ε)² = 2πa² [√ (1-ε²)]/T a² (1-ε) ²; θ'(0, 0) = 2π [√ (1-ε²)]/T (1-ε) ² θ'(0,t) = {2π[√(1-ε²)]/T(1-ε)²}Exp{-2[ω(m) + ω(r)]t θ'(0,t) = {2π[√(1-ε²)]/(1-ε)²}{cos 2[ω(m) + ω(r)]t - ỉ sin 2[ω(m) + ω(r)]t} θ'(0,t) = θ'(0,0) {1- 2sin² [ω(m) + ω(r)]t - ỉ 2isin [ω(m) + ω(r)]t cos [ω(m) + ω(r)]t} θ'(0,t) = θ'(0,0){1 - 2[sin ω(m)t cos ω(r)t + cos ω(m) sin ω(r) t]²} - 2ỉ θ'(0, 0) sin [ω (m) + ω(r)] t cos [ω (m) + ω(r)] t Δ θ (0, t) = Real Δ θ (0, t) + Imaginary Δ θ (0.t) Real Δ θ (0, t) = θ'(0, 0) {1 - 2[sin ω (m) t cos ω(r) t + cos ω (m)t sin ω(r)t]²} W(ob) = Real Δ θ (0, t) - θ'(0, 0) = - 2 θ'(0, 0){(v°/c)√ [1-(v*/c) ²] + (v*/c)√ [1- (v°/c) ²]}² v ° = spin velocity; v* = orbital velocity; v°/c = sin ω (m)t; v*/c = cos ω (r) t v°/c << 1; (v°/c)² ≈ 0; v*/c << 1; (v*/c)² ≈ 0 W (ob) = - 2[2π √ (1-ε²)/T (1-ε) ²] [(v° + v*)/c] ² W (ob) = (- 4π /T) {[√ (1-ε²)]/ (1-ε) ²} [(v° + v*)/c] ² radians W (ob) = (-720/T) {[√ (1-ε²)]/ (1-ε) ²} [(v° + v*)/c] ² degrees; Multiplication by 180/π W° (ob) = (-720x36526/T) {[√ (1-ε²)]/ (1-ε) ²} [(v°+ v*)/c] ² degrees/100 years W” (ob) = (-720x26526x3600/T) {[√ (1-ε²)]/ (1-ε) ²} [(v° + v*)/c] ² seconds /100 years The circumference of an ellipse: 2πa (1 - ε²/4 + 3/16(ε²)²- --.) ≈ 2πa (1-ε²/4); R =a (1-ε²/4) v (m) = √ [GM²/ (m + M) a (1-ε²/4)] ≈ √ [GM/a (1-ε²/4)]; m<<M; Solar system v (M) = √ [Gm² / (m + M)a(1-ε²/4)] ≈ 0; m<<M Application 3: Advance of Perihelion of mercury. G=6.673x10^-11; M=2x10^30kg; m=.32x10^24kg; ε = 0.206; T=88days c = 299792.458 km/sec; a = 58.2km/sec; 1-ε²/4 = 0.989391 ρ (m) = 0.696x10^9m; ρ(m)=2.44x10^6m; T(sun) = 25days v° (M) = 2km/sec ; v° = 2meters/sec v *= v(m) = √ [GM/a (1-ε²/4)]; v(M) = √[Gm²/(m + M)a(1-ε²)] ≈ 0 v°(m) = 2m/sec (Mercury) v°(M)= 2km/sec(sun) Calculations yields: v = v* + v° =48.14km/sec (mercury); [√ (1- ε²)] (1-ε) ² = 1.552 W" (ob) = (-720x36526x3600/T) {[√ (1-ε²)]/ (1-ε) ²} (v/c) ² W" (ob) = (-720x36526x3600/88) x (1.552) (48.14/299792)² = 43.0”/century Application 4: Gravitational red shift: Pound Rebka Experiment r (θ, t) = r(θ, 0) Exp [î w(r)t] = λ(r) Exp[ỉ ω(r)t]; λ(r) = 0 1/r(θ, t) = 1/r(θ,0) = (1/λ) {Exp [-(î wt)]} υ (θ, t) = υ (θ,0) υ(0, t) = υ (θ, 0) Exp (-ì wt) = υ (θ, 0) [cos (ω t) + ỉ sin (ω t)] sin ω(r)t = v/c; cos ω(r)t = √[1-(v/c)²] υ (0,t) = υ(0,0){√[1-(v/c)²] + ỉ (v/c)} = Real {υ(0, t)} + Imaginary{υ(0, t)} Real {υ (0, t)} = υ (0, 0) √ [1-(v/c) ²] ≈ υ (0, 0) [1 - 1/2(v/c) ²] Δ υ (0, t) = real {υ (0, t)} - υ (0, 0) Δ υ (0, t) = -υ (0, 0)/2 [(v/c) ²] Δ υ(0, t)/υ(0, 0) = -1/2(v/c)²[up]-{1/2(v/c)²[down]} = - (v/c) ² v² = 2gh=2(9.806) (22.6m) Δ υ/υ [Total]=[2x9.806x22.6/299792.458]=4.93169x10^-15 Observed value: 5.1±5x10^-15 5- Light bending: Lord Eddington experiment θ' (θ, t) = θ' (θ, 0) θ'(0, t) = [h/r²(θ,0)] Exp { -2ỉ[ ω(m) + ω(r)]t}; ω (m) = 0 θ '(θ, t) = [2A/tr²(θ, 0)]{1 - 2sin²ω(r)t - 2ỉ sin ω(r)t cos ω(r)t} [t θ'(θ, t)] = [2A/r²(θ' 0)][1 - 2sin²ω(r)t] -2ỉ[2A/r²(θ, 0)][sin ω(r)t cos ω(r)t] = Δ x + i Δ y Δ θ = Δ x - [A/r² (θ, 0)] = - [A/r²(θ, 0)][4sin²ω(r)t]; sin ω(r)t = v/c Δ θ = - [A/r²(θ, 0)](v/c) ² (v/c)² ≈ 1.75"; v² = GM/R; G = Gravitational constant; M = Sun mass; R = sun radius Δ θ = [A/r²(θ, 0)] [1.75"]; A = area The values depend on near by stars and the measured values fit this equation. Russians in 1936; Δ θ = 2.74 [A/r² (θ, 0)] = π/2 Δ θ = π/2(1.75") = 2.74" Application 6: Shapiro time delay (Vikings 6, 7; 1977) Mars --------------------------- Middle---- Sun ------------- Earth The center of mass is the sun. The sun produces a velocity field given by v = √ [GM/a (1- ε²/4)] From above t =2 arc length/c=2d Δ w/c = (8π r/c) (v/c) ²; Δ w=4π (v/c) ²; r = 2a=d t = 16πGM/c³ (1-ε²/4); ε = [a (1) -a(2)]/[a(1) + a(2)] = .2075 t = (8πd/c) (v/c) ²= 8π (377,536,987.5/299792.458) (26.6575872/299792.458)²=250μs If d = 2a (1-ε²/4), then t = 247.597μs value theorized actual measured value is 250μs All this is not due to space-time but due to light aberration caused by moving planets. θ'(0,0) = h(0,0)/r²(0,0) = 2π/T θ' (0,t) = θ'(0,0)Exp(-2ỉwt)={2π/T} Exp (-2iwt) θ'(0,t) = θ'(0,0) [cosine 2(wt) - ỉ sine 2(wt)] = θ'(0,0) [1- 2sine² (wt) - ỉ sin 2(wt)] θ'(0,t) = θ'(0,t)(x) + θ'(0,t)(y); θ'(0,t)(x) = θ'(0,0)[ 1- 2sine² (wt)] θ'(0,t)(x) – θ'(0,0) = - 2θ'(0,0)sine²(wt) = - 2θ'(0,0)(v/c)² v/c=sine wt; c=light speed T [θ'(0, t) - θ'(0, 0)] = -4π (v/c) ²} Δ θ = -4π (v/c) ² Earth-Mars Sun-Photon: The circumference of an ellipse: 2πa (1 - ε²/4 + 3/16(ε²)²---) ≈ 2πa (1-ε²/4); R =a (1-ε²/4) v=√ [Gm M/ (m + M) a (1-ε²/4)] ≈ √ [GM/a (1-ε²/4)]; m<<M; Solar system ΔΓ = 2 arc length/c = 2[Δ θ] 2d/c = 2[- 4π (v/c) ²] 2d/c; ΔΓ = -8πd/c (v/c) ²; ΔΓ = 8πd/c³ [GM/a (1-ε²/4)] =16πGM/c³ (1-ε²/4) = Γ0 (1 - ε²/4) ε = [a (planet 1) - a (planet 2)]/ [a (planet 1) + a (planet 2)] =0.2075 Mars-Earth Γ0 = 16 πGM/c³= 247.5974607μs=universal constant; ΔΓ = 250μs Mars-Earth.