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Independent News, Research, Scientific Analysis, and Commentary on the Smolensk Crash and its Implications.

  • Antoni Macierewicz, Vice Chairman of the Law and Justice Party (PiS)Chairman of the Polish Government Re-Investigation Commission of the Crash of Polish Air Force One on April 10, 2010 in Smolensk
  • Russian Image Management by Euguene PoteatRetired CIA Senior Scientific Intelligence Officer Euguene Poteat speaks out
  • Smolensk Crash DisinformationNo one saw anything, no one heard anything, no one filmed anything ...
  • TNT and other explosives detected on the wreckage of Polish presidential planeC4, TNT, RDX, HMX (octogen), p-MNT and Nitroglycerine detected ...
  • Smolensk Crash related deaths"The Serial Suicider" Strikes Again. Key witness dead!
  • Countdown to the crash of Flight PLF101Countdown to the crash of Polish Governement Tupolev TU-154M flight PLF101.
  • Smolensk Widow Beata Gosiewska exposes the Smolnesk Crash LieSmolensk Crash Widow exposes the "Smolensk Lie"
  • The List of 96 Victims of Polish Air Crash In Smolensk, Russia, on April 10, 2010.The list of 96 victims
  • 9 Questions for Professor Binienda.Is the U.S. scientific community interested in the Smolensk crash?
  • Lech Kaczynski's Security Was Purposefully CompromisedPolish president's security was purposefully compromised!
  • Slide 11 Title Goes HereThe main causes of the Polish Tu-154M crash were two explosions onboard.
  • Facts presented in this report demonstrate a clear and convincing evidence of obstruction of justice in the one-sided and superficial investigation that violates basic norms of any airplane crash investigation, elementary standards of due process of law, and rights of the families of the victims.Was the official investigation an obstruction of justice?
Chairman of the Polish Government Re-Investigation Commission of the Crash of Polish Air Force One on April 10, 2010 in Smolensk Russian Image Management by Retired CIA Senior Scientific Intelligene Officer, Eugene Poteat, LL.D Smolensk Crash Disinformation Explosives Found on the wreckage of Polish Air Force One. Coverup by Suicide Smolensk Crash Timeline Smolensk Crash Lie Exposed. Smolensk Crash Victims 9 Questions for Dr. Binienda. Polish president's security was intentionally compromised. Scientific analysis of Smolensk crash points to the invalidity of the official findings. 2014 independent Smolensk Crash Raport: What do we know about Smolensk crash today.

Some Mechanical and Structural Aspects of the Smolensk Crash
By Dr. Gregory Szuladzinski, Ph.D., MSME
SCND2014GS

Appendix V. Aircraft Rotation around the Longitudinal Axis

The rolling began near critical point K and was due to loss of lift on the wing. The following calculation is approximate and simplified. The inertia data of the aircraft is assumed constant in spite of the accident, during which the lift force vanishes on the left wing together with the loss of part of that wing.

Takeoff mass: M0 = 110.5 t

mass at point K: M = 78.6 t

moment of inertia around the longitudinal axis, at startup: I0 = 1928 t-m2

moment of inertia around the longitudinal axis, point K: I = 1371 t-m2

(Assumed in proportion to the mass)

estimated lift force on the wing P ≈ 0.4 Mg = 0.4x78, 600x9.81 = 308,400 N

estimated distance of the center of aero of the wing from longitudinal axis: r = 8.2 m

Wing moving upwards (right) will develop less lift than the same wing in normal flight, because it reduces the effective angle of attack. Here we assume a loss of 20%.

torque M = 0.8Pr = 0.8x308,400x8.2 = 2.023 x106 Nm

angular acceleration: ε = M / I = 1.476 rad/s2

the time t it takes the turn by the angle θ: θ = εt2 / 2, i.e. for θ = 90°:

Over time, the state of affairs will change and it is unlikely that such acceleration could be continued. Therefore, we assume that the angle of 90° above the angular velocity is constant:

ω = ε t =1.476x1.459 = 2.153 rad/s

time to reach 1200 : (Δθ=30°), Δt = Δθ/ω = 0.243 s, t120 = 1.459 + 0.243 = 1.70 s

time to reach 200°: (Δθ=110°), Δt = Δθ/ω = 0.892 s, t200 = 1.459 + 0.892 = 2.35 s

One can obtain more precise results if, instead of the above intuitive assumptions, one uses more accurate data that can be obtained from the aerodynamic simulation.

According to the MAK report, the time to reach the turn of 2000 was 6 s, but it is unclear whether this time was calculated in a manner consistent with this calculation. Of course, if not all of the lift on the wing has lost, turning was slower than the above shows and the calculated time would be longer.

 

Parts of this Report
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Explosives Found on the Wreckage

Conclusive evidence of explosives detection emerges! Antoni Macierewicz Press Conference, July 19, 2013. Examples of Spectrometer readouts released to the public.

Conclusive evidence of explosives detection emerges! Antoni Macierewicz Press Conference, July 19, 2013. Examples of Spectrometer readouts released to the public.

Read more here

 

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