how the universal bird lifts
By Henryk Szubinski
freedoom of knowledge 5th law 5th framework Chordis6
positive 6th law:
A BREAK VALUE IN SHEER OF EVERYTHING THAT CAN BE USED TO ALTER THE BALANCE ON LIFTABILITY OF ANY MASS IN ANY VECTOR VALUE:
x function or gap:
In physical cosmology, the large-scale structure of the universe refers to the characterization of observable distributions of matter and light on the largest scales (typically on the order of billions of light-years). Sky surveys and mappings of the various wavelength bands of electromagnetic radiation (in particular 21-cm emission) have yielded much information on the content and character of the universe‘s structure. The organization of structure appears to follow as a hierarchical model with organization up to the scale of superclusters and filaments. Larger than this, there seems to be no continued structure, a phenomenon which has been referred to as the “End of Greatness”.
THIS DEPENDS IN LARGE TO WHAT FLEW:
SOME CONCEPT SIMILARITY OF THE GREAT WALL TO A BIRDS TAKEOFF:
data on the multi linears of the tail view shows the process of increased mobility:
what happened:
The Sloan Great Wall is a giant wall of galaxies (a galactic filament), which is as of 2009 the largest known structure in the Universe. Its discovery was announced on October 20, 2003 by J. Richard Gott III and Mario Jurić, of Princeton University, and their colleagues, based on data from the Sloan Digital Sky Survey.[1] The wall measures 1.37 billion light years in length and is located approximately one billion light-years from Earth.
The Sloan Great Wall is nearly three times longer than the Great Wall of galaxies, the previous record-holder, which was discovered by Margaret Geller and John Huchra of Harvard in 1989.
The Sloan Great Wall is classified as hypercluster SCl 126 in SIMBAD
the sloan appearance from the top view
with the format of F1,F2,.F3,F4,F5,F6,F7 ………and so on where lim x =infinite
the data on the usage of a type shute that can rotate to define the basics of our position in the universe by using the differences of the top shute to the base shute in a time computation of the differences:
as any positional differencial input = access to data on anything
on a plane with the top views of what occurs as the wing tipps lift forwards and the planarity of its memory is reduced to the pull out of the plane onto which to land :
WHAT HAPPENS WHEN THE BREAK ZONE IS IN A MULTIPLE RELATION WITH THE EFFECTS OF A BREAK LIFT SPACETIME:
F1 , F2, .F3, F4, F5 ,F6, F7
Figure 1.3. Normal stress in a prismatic bar. The stress or force distribution in the cross section of the bar is not necessarily uniform. However, an average normal stress can be used
This side view might be the demonstration of what is occuring in the general mass alterations of the lift and pull of the underside surface at a angle of 330 degrees to the general lift angle of 200 degrees of the general sloan look:
the basics of the break in sheer planes is shown in its ready format at the alterations of 90 degrees to the 2 nd quadrance:
Figure 1.4. Shear stress in a prismatic bar. The stress or force distribution in the cross section of the bar is not necessarily uniform. However, an average shear stress is not a good approximation.
First the simple case of a prismatic bar subjected to an axial force will be examined. These axial forces can be produced either by tension or compression (Figures 1.2 and 1.3). Considering a cross sectional area perpendicular to the axis of the bar, from the equilibrium of forces the resultant normal force can be found. The intensity of internal forces, or stress , in the cross sectional area can then be obtained by dividing the total normal force , e.g. tensile force if acting outward to the plane or compressive force if acting inward to the plane, by the cross-sectional area where it is acting upon. In this case the stress is a scalar quantity called engineering or nominal stress that represents an average stress () over the area, i.e. the stress in the cross section is uniformly distributed. Thus, we have
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A different type of stress is obtained when transverse forces are applied to the prismatic bar as show in Figure 1.4. Considering the same cross section as before, from static equilibrium, the internal force has a magnitude equal to and in opposite direction parallel to the cross section. is called the shear force. Dividing the shear force by the area of the cross section we obtain the shear stress. In this case the shear stress is a scalar quantity representing an average shear stress () in the section, i.e. the stress in the cross section is uniformly distributed.
basically like a hoop the values in dimensional perspective the top hoop is larger so that the conservations of force in spacetime are directly visible in the process by which conservation of flow is based on the low hoop as a lower value: the dynamics of the whole process is from a state in unrest to a state of unrest:
with the dynamics flow of the levels in their similar space time area planarity..
THE RESULTANT DATA ON ANYTHING CAN ALSO BE USED WITH THE SMOOTH TRIANGULATIONS OF HOW A PROGRAMME A.I FOR THE STRUCTURISATIONS OF EVERY DIFFERENCIAL IN THE VALUES OF INVERSIONS ARE BASED ON DIRECT IMAGERY AND DETAIL PROGRAMMES:
THE STRESS PROBLEM OF LIFT IS BASIC: THE STRESS PLANE ON 1) as the connective vector directions in opposite directions to form a gap in the measure of connectives and as such to define the break as lift space balance:
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In general, however, the stress is not uniformly distributed over the cross section of a material body, and consequently the stress at a point on a given area is different from the average stress over the entire area. In Figure 1.3, the normal stress is observed in two planes and of the axially loaded prismatic bar. The stress on plane , which is closer to the point of application of the load , varies more across the cross section than that of plane . However, if the cross sectional area of the bar is very small, e.g. a slender bar, the variation of stress across the area is small and the normal stress can be approximated by . On the other hand, the variation of shear stress across the section of a prismatic bar cannot be assumed uniform.
Therefore, it is necessary to define the stress at a specific point in the surface.
processing the data on values of the base accertiuons of the electron mass of a H2O type buoyancy in the responses to the frontal turbines being electron lifters in a STRING:
data as the specific formats of the preliminary study of the values in their responsive requirements for data on the high sinusodial format of the tail hemi volumes and their general effct on String theory that accompanies a higher attract by magnetism thatn the value of a electron mass dropping from the supercharged hemi formats . Giving the break —–>floor a touch at a 3 x or larger electron response by fall as is with strings the basics of the sinusodial rebalance of the electron doing its own fall lifting as such a stable format:
data on tthe specifics of the generations of turbines and their responsive multiple inteke increases by
3x = the values in front of and to the tail as
being in exact similarity of gravity by the involvances of mass to SOH values and the cut off rates of the forward sectional generations in the thump of the break zone;
MOST OF THE DATA IS ON THE EXPANSIONS OF tail sections into large hemi spherical formats; the opposite on the nose by multiple breakups on the values of generators and power by turbines:
3(1/2+x) =(Vol / 100 )y