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Kristy Noem “Evil BITCH Series” Trailer
Duration: 1:14
Views: 14
Submitted: 1 day ago
Submitted by:
Description:
Yes I have secretly been producing a series called “Kristy Noem Evil Bitch” and it is only going to be available on my streaming platform…
“I choose to spend MY LIFE chasing down Lions and Cougars who devour the innocent…”
-Stateless Warrior
What do I THINK of her ACTUAL IQ?
Sewage RODENT equal!
But I don’t allow idiots to hold humanity back on my sites so the way to move forward is to IGNORE THEM!
It’s like this, all humans want a safe flying car but are too stupid to engineer it using the correct propulsion system which is stable even in high winds so I’m going to reveal here for the first time ever because you can retrofit Electric cars with this propulsion system and literally get humans conditioned to flight and TRANSITION EVERY MAJOR CITY IN THE WORLD
TODAY, into a FLYING CAR CAPITAL using “Cycloidal Propulsion” for super safe “Flying Electric Cars” so I’m a take you on the physics and mathematics dive so you could grasp this subject well regardless of how dumb American federal government allowed ONE IDIOT to transform it into a fascist Gestapo with this low IQ’d whore as it’s Gestapo command executive so let’s leave this low IQ’d g-how of USA in rear view mirror as I will get back to addressing her low IQ’d issues with my SICARIO Ai satire but meanwhile laser focus on “Physics of Urban Air Mobility!”
Conventional electric vertical takeoff and landing (eVTOL) designs face fundamental limitations rooted in their propulsion physics which I find Engineering ticks WORTHY so total Las Vegas show material! What I mean is that atandard propellers and rotors require vehicle tilting for directional control, introducing significant inertia that slows maneuverability and creates passenger discomfort… But cycloidal propulsion is a physics-driven solution where advantages in agility, control, and efficiency derive directly from its unique operational principles and mathematical foundations because cycloidal propulsion system consists of multiple blades rotating around a central axis within a cylindrical housing. Each blade simultaneously undergoes two motions: revolution around the axis and continuous pitch variation about its own axis. The mathematical heart of this system lies in the blade pitch kinematics, where the blade pitch angle θ is not constant but a function of its angular position ψ around the cycle. So I would MODEL this relationship as: θ(ψ) = θ₀ + Θ sin(ψ - φ). Here, θ₀ represents the mean pitch offset, Θ controls the amplitude of the pitching motion which determines thrust magnitude, and φ represents the phase angle which serves as the critical control parameter that instantly sets the direction of the net thrust vector in the 360-degree plane. By adjusting this phase angle φ, the system shifts the point in the rotational cycle where each blade presents its maximum angle of attack, thereby redirecting the net aerodynamic force without moving any large structures. Americans and Chinese flying car engineering I find to be flawed and complete GARBAGE which after analyzing make me wannuh vomit cause both SUCK at getting their math and physics right! The aerodynamic forces on a cycloidal rotor blade element however, differ fundamentally from conventional propellers due to unsteady flow conditions. Each blade element experiences a relative wind velocity W composed of its rotational velocity and the vehicle's forward speed. The elemental lift dL and drag dD are given by: dL = ½ ρ W² c Cl dγ and dD = ½ ρ W² c Cd dγ, where ρ is air density, c is chord length, Cl and Cd are lift and drag coefficients respectively, and dγ is the spanwise element length. The rapid pitching motion inherent to cycloidal systems delays flow separation through unsteady aerodynamic effects, allowing operation at effectively higher angles of attack and achieving greater maximum lift coefficients than possible in steady flow, particularly at low Reynolds numbers. This phenomenon contributes significantly to the high thrust density characteristic of cycloidal rotors so what I mean is for example, hover efficiency metrics, cycloidal rotors will have superior performance quantified through the “Figure of Merit” (FM), which compares actual power required to “ideal power” and cycloidal rotors would achieve higher power loading (thrust per unit power) at equivalent disk loading (thrust per unit area) compared to conventional rotors, indicating higher FM values so my question is if American and Chinese engineers are so bright, how come you can’t engineer to achieve IDEAL POWER? It appears that both Chinese and Americans are basic copycats v 1.9 stealing each others designs too stupid to attain “IDEAL thrust POWER!
How is cycloidal superior? Efficiency advantage stems from two primary factors: the entire blade span operates at similar velocities enabling uniform aerodynamic optimization, and the exploitation of unsteady aerodynamic effects that enhance lift production. Key performance parameters include the advance ratio J = V/(ωR), representing the ratio of forward flight speed V to rotor tip speed ωR. Cycloidal rotors maintain efficiency across higher advance ratios than Police helicopters in American City skies which face limitations from retreating blade stall. The phase angle φ directly controls thrust direction while pitch amplitude Θ governs thrust magnitude. Power loading T/P measures hover efficiency, with cycloidal systems demonstrating superior values compared to conventional rotellers at equivalent disk loading. As a matter of fact, I could see why low IQ’d CHINESE AND AMERICAN mechanical implementation of cycloidal propulsion hasn’t been forthcoming and implement presents unique engineering challenges to both nations engineers particularly regarding centrifugal force management because unlike helicopter blades that primarily experience axial tension (If you notice while observing American Police or other helicopters in flight) cycloidal rotor blades undergo significant centrifugal loads in bending, creating substantial structural design considerations but there are three primary support configurations: the "T" shape with single central support (shortest main shaft but largest blade deflection), the "n" shape with supports at both ends (longest main shaft with vibration concerns), and the "pi" shape with two supports along the span. The "pi" configuration proves optimal, with mathematical analysis demonstrating minimum blade deflection occurs when the support distance is approximately 56% of the total blade span, effectively balancing weight, stiffness, and vibration requirements. Pitch control mechanisms can easily be modded with high-friction cam systems or sophisticated multi-bar linkage arrangements that enable all blades to be controlled through a single shared eccentric ring, reducing mechanical complexity and weight. These systems must precisely maintain the sinusoidal pitch relationship while withstanding significant dynamic loads.
And I stop right here despite having ability to write a thousand page book on this engineering solution because this is a satire fake news site with occasional interjections of my cutting edge engineering solutions which can easily pave the way for elevation of human life on Earth so you can leave idiots repressive idiots like Kristy Noem on the ground where she belongs!
Yo, AMERICAN ENEMY STALKER AGENT G-FAGGOTS AND CUNTS:
I’m hoing to MOTHER FUCK YOUR ASIAN AND “CRACKER AGENT CUNTS” BITCH PITCHIN AMERICAN BORN UTTERLY WORTHLESS G-CUNT SHIT OUT BASTARD BRATS!
I don’t date American ENEMY STALKER cunts and whores nut best of luck enhineering a social hack when you get me eamerican enemy pussy whipped! I don’t allow American ENEMY G-FAGGOT AGENT AND CUNT idiots to alter my family UNIT to their governments benefit and I have intentionally ABSTAINED from revealing actual formula on how to turn any electric “FOUR WHEEL DRIVE CAPABLE” car into a flying car which can EASILY withstand high winds and would be far safer than any piece of shit American shit engineered Aircraft cause even Boeing 787 is an engineering FUCKUP!
“American enemy low IQ’d bastard idiots belong stuck on Earth!”
Besides that: on 12/06/2017 you American g-fags and cunts carried out my mothers abduction, tortured her with microwave energy weapons in ABSOLUTE ISOLATION, sexually abused her, and if any of you ever come to me for any service, assistance, enlistment I WILL PERSONALLY KILL YOUR AMERICAN ENEMY AGENTS B4 you can ever reach for that fuckin sidearm…
Furthermore; all your American enemy whores you deploy as honey bait, I’ll personally shoot up with Sinaloa Heroin to turn them into lifelong cocksuckers
This never goes away… It will NEVER END…
When you die, your grown adult children will have a bulls eye on their fucked asses… When they check out it will be your grandchildren…
If I’m ever on your American enemy filthy fuckin base,THE ONLY THING I’D BE DOING IS KILLING YOUR ENEMY SODIERS AT ABSOLUTE FUCKIN RANDOM!
Ya’ll agent g-fags and cunts have serious memorization issues… Forgot what I promised you on 12/09/2017?
Good luck American enemy g-faggot agent stalker faggots and
Cunts, you’ll need it…
https://www.myvideotime.com/video/188/full-video-footage-of-my-mothers-abduction-captured-on-12-06-2017/
Wannuh try your American enemy cunt bitches wit’chuh bastard fuckin brats pitchin fuh cognitive pussy bond to USA?
MOTHER FUCK ALL YOUR BITCHES AND FUCKIN BRATS THEY SHIT THE FUCK OUT CAUSE THERE IS NOTHING I WOULD LOVE TO BE MORE THAN ABORTION DOC SO I CAN THROW YOUR MOTHER FUCKED LITTLE BASTARDS ALL INTO A TRASH BAG AND IN INCINERATE THEM EVERY SINGLE DAY!
NOTHING GETS MY DICK ROCK HARD FASTER THAN ONE MILLION ANORTIONS ON AMERICAN ENEMY BTICH ASS MOTHER FUCKED STALKER AGENT G-FAGGOT AND CUNT SOIL!
Stateless Warrior
“I choose to spend MY LIFE chasing down Lions and Cougars who devour the innocent…”
-Stateless Warrior
What do I THINK of her ACTUAL IQ?
Sewage RODENT equal!
But I don’t allow idiots to hold humanity back on my sites so the way to move forward is to IGNORE THEM!
It’s like this, all humans want a safe flying car but are too stupid to engineer it using the correct propulsion system which is stable even in high winds so I’m going to reveal here for the first time ever because you can retrofit Electric cars with this propulsion system and literally get humans conditioned to flight and TRANSITION EVERY MAJOR CITY IN THE WORLD
TODAY, into a FLYING CAR CAPITAL using “Cycloidal Propulsion” for super safe “Flying Electric Cars” so I’m a take you on the physics and mathematics dive so you could grasp this subject well regardless of how dumb American federal government allowed ONE IDIOT to transform it into a fascist Gestapo with this low IQ’d whore as it’s Gestapo command executive so let’s leave this low IQ’d g-how of USA in rear view mirror as I will get back to addressing her low IQ’d issues with my SICARIO Ai satire but meanwhile laser focus on “Physics of Urban Air Mobility!”
Conventional electric vertical takeoff and landing (eVTOL) designs face fundamental limitations rooted in their propulsion physics which I find Engineering ticks WORTHY so total Las Vegas show material! What I mean is that atandard propellers and rotors require vehicle tilting for directional control, introducing significant inertia that slows maneuverability and creates passenger discomfort… But cycloidal propulsion is a physics-driven solution where advantages in agility, control, and efficiency derive directly from its unique operational principles and mathematical foundations because cycloidal propulsion system consists of multiple blades rotating around a central axis within a cylindrical housing. Each blade simultaneously undergoes two motions: revolution around the axis and continuous pitch variation about its own axis. The mathematical heart of this system lies in the blade pitch kinematics, where the blade pitch angle θ is not constant but a function of its angular position ψ around the cycle. So I would MODEL this relationship as: θ(ψ) = θ₀ + Θ sin(ψ - φ). Here, θ₀ represents the mean pitch offset, Θ controls the amplitude of the pitching motion which determines thrust magnitude, and φ represents the phase angle which serves as the critical control parameter that instantly sets the direction of the net thrust vector in the 360-degree plane. By adjusting this phase angle φ, the system shifts the point in the rotational cycle where each blade presents its maximum angle of attack, thereby redirecting the net aerodynamic force without moving any large structures. Americans and Chinese flying car engineering I find to be flawed and complete GARBAGE which after analyzing make me wannuh vomit cause both SUCK at getting their math and physics right! The aerodynamic forces on a cycloidal rotor blade element however, differ fundamentally from conventional propellers due to unsteady flow conditions. Each blade element experiences a relative wind velocity W composed of its rotational velocity and the vehicle's forward speed. The elemental lift dL and drag dD are given by: dL = ½ ρ W² c Cl dγ and dD = ½ ρ W² c Cd dγ, where ρ is air density, c is chord length, Cl and Cd are lift and drag coefficients respectively, and dγ is the spanwise element length. The rapid pitching motion inherent to cycloidal systems delays flow separation through unsteady aerodynamic effects, allowing operation at effectively higher angles of attack and achieving greater maximum lift coefficients than possible in steady flow, particularly at low Reynolds numbers. This phenomenon contributes significantly to the high thrust density characteristic of cycloidal rotors so what I mean is for example, hover efficiency metrics, cycloidal rotors will have superior performance quantified through the “Figure of Merit” (FM), which compares actual power required to “ideal power” and cycloidal rotors would achieve higher power loading (thrust per unit power) at equivalent disk loading (thrust per unit area) compared to conventional rotors, indicating higher FM values so my question is if American and Chinese engineers are so bright, how come you can’t engineer to achieve IDEAL POWER? It appears that both Chinese and Americans are basic copycats v 1.9 stealing each others designs too stupid to attain “IDEAL thrust POWER!
How is cycloidal superior? Efficiency advantage stems from two primary factors: the entire blade span operates at similar velocities enabling uniform aerodynamic optimization, and the exploitation of unsteady aerodynamic effects that enhance lift production. Key performance parameters include the advance ratio J = V/(ωR), representing the ratio of forward flight speed V to rotor tip speed ωR. Cycloidal rotors maintain efficiency across higher advance ratios than Police helicopters in American City skies which face limitations from retreating blade stall. The phase angle φ directly controls thrust direction while pitch amplitude Θ governs thrust magnitude. Power loading T/P measures hover efficiency, with cycloidal systems demonstrating superior values compared to conventional rotellers at equivalent disk loading. As a matter of fact, I could see why low IQ’d CHINESE AND AMERICAN mechanical implementation of cycloidal propulsion hasn’t been forthcoming and implement presents unique engineering challenges to both nations engineers particularly regarding centrifugal force management because unlike helicopter blades that primarily experience axial tension (If you notice while observing American Police or other helicopters in flight) cycloidal rotor blades undergo significant centrifugal loads in bending, creating substantial structural design considerations but there are three primary support configurations: the "T" shape with single central support (shortest main shaft but largest blade deflection), the "n" shape with supports at both ends (longest main shaft with vibration concerns), and the "pi" shape with two supports along the span. The "pi" configuration proves optimal, with mathematical analysis demonstrating minimum blade deflection occurs when the support distance is approximately 56% of the total blade span, effectively balancing weight, stiffness, and vibration requirements. Pitch control mechanisms can easily be modded with high-friction cam systems or sophisticated multi-bar linkage arrangements that enable all blades to be controlled through a single shared eccentric ring, reducing mechanical complexity and weight. These systems must precisely maintain the sinusoidal pitch relationship while withstanding significant dynamic loads.
And I stop right here despite having ability to write a thousand page book on this engineering solution because this is a satire fake news site with occasional interjections of my cutting edge engineering solutions which can easily pave the way for elevation of human life on Earth so you can leave idiots repressive idiots like Kristy Noem on the ground where she belongs!
Yo, AMERICAN ENEMY STALKER AGENT G-FAGGOTS AND CUNTS:
I’m hoing to MOTHER FUCK YOUR ASIAN AND “CRACKER AGENT CUNTS” BITCH PITCHIN AMERICAN BORN UTTERLY WORTHLESS G-CUNT SHIT OUT BASTARD BRATS!
I don’t date American ENEMY STALKER cunts and whores nut best of luck enhineering a social hack when you get me eamerican enemy pussy whipped! I don’t allow American ENEMY G-FAGGOT AGENT AND CUNT idiots to alter my family UNIT to their governments benefit and I have intentionally ABSTAINED from revealing actual formula on how to turn any electric “FOUR WHEEL DRIVE CAPABLE” car into a flying car which can EASILY withstand high winds and would be far safer than any piece of shit American shit engineered Aircraft cause even Boeing 787 is an engineering FUCKUP!
“American enemy low IQ’d bastard idiots belong stuck on Earth!”
Besides that: on 12/06/2017 you American g-fags and cunts carried out my mothers abduction, tortured her with microwave energy weapons in ABSOLUTE ISOLATION, sexually abused her, and if any of you ever come to me for any service, assistance, enlistment I WILL PERSONALLY KILL YOUR AMERICAN ENEMY AGENTS B4 you can ever reach for that fuckin sidearm…
Furthermore; all your American enemy whores you deploy as honey bait, I’ll personally shoot up with Sinaloa Heroin to turn them into lifelong cocksuckers
This never goes away… It will NEVER END…
When you die, your grown adult children will have a bulls eye on their fucked asses… When they check out it will be your grandchildren…
If I’m ever on your American enemy filthy fuckin base,THE ONLY THING I’D BE DOING IS KILLING YOUR ENEMY SODIERS AT ABSOLUTE FUCKIN RANDOM!
Ya’ll agent g-fags and cunts have serious memorization issues… Forgot what I promised you on 12/09/2017?
Good luck American enemy g-faggot agent stalker faggots and
Cunts, you’ll need it…
https://www.myvideotime.com/video/188/full-video-footage-of-my-mothers-abduction-captured-on-12-06-2017/
Wannuh try your American enemy cunt bitches wit’chuh bastard fuckin brats pitchin fuh cognitive pussy bond to USA?
MOTHER FUCK ALL YOUR BITCHES AND FUCKIN BRATS THEY SHIT THE FUCK OUT CAUSE THERE IS NOTHING I WOULD LOVE TO BE MORE THAN ABORTION DOC SO I CAN THROW YOUR MOTHER FUCKED LITTLE BASTARDS ALL INTO A TRASH BAG AND IN INCINERATE THEM EVERY SINGLE DAY!
NOTHING GETS MY DICK ROCK HARD FASTER THAN ONE MILLION ANORTIONS ON AMERICAN ENEMY BTICH ASS MOTHER FUCKED STALKER AGENT G-FAGGOT AND CUNT SOIL!
Stateless Warrior
