sci fi reality…eco strategy.clearing the interactive resistances of safe couplings

 LOCALISING WATER ELECROLYSIS OR WATER ADVANCED FORMATS FOR POWER IN THE LITHUANIAN / SWEDISH AREA:

By Henryk Szubinski

inverting the ecological problems

where productivity is bason non value in descriptives of industrial usage:

a world in exterior developments met with the paralysis of the wall plugg in stemmic relationships of force:

FULL EARTH DEENVELOPMENTAL EXPANSIONS IN THE PROCESS TO NEUTRALISE PROBLEMS IN ECOLOGY:

File:WorldMap PlugTypeInUse.png

plug problem

DEALING with wall sockets as a format ofpoint hazzards on continental laue of areas and their predefined input hazzard by using the depth perceptions of a pre internal format for defning the interflow of externals of each continents hazzardoud values and the internal responses on the values of the point opposition by the format over implied level of interval extra dimensionality by the usage of a depth gauger on a process by which the value is implied to be as similar to the data required to be implicative of a sustainable value in the exchange of data as the response that the bio system has aquuired a format for singgular responsivity..

By Henryk Szubinski

clearing the interactive resistances of safe couplings

File:CEE 7-17 plug.jpg

WHEN THE FORMAT FOR A PREDICATBLE BLOCKAGE OF THE INTERACTIVE FORMATS OF APPROACH TO A EXTERNAL ECOLOGICAL PROBLEM ARE BASED ON THE DATA OF A NON VALUE INPUT TO EGEGE SAFE INTERACTIONS , THE PROBLEM IS DEFINED AS A  FORMAT OF USAGE OF THOOSE DARK VECTORS AS 10 X =THE BASIC VALUES TO PREEMPT THE DATA ON EXCHANGES BY THE USAGE OF THE LOW LEVEL PROXIMITY TO A VALUE INTERACTION BASED ON A HIGHER VELOCITY COUPLING TO DATA ON ANY VALUE BY THE USAGE OF THE OPPOSITIONS OF DATA BY INVERTIONS

A OPPOSED 10 Y VACTOR VALUE AS THE INTERACTIONS OF

10 X =10 Y IS A BASIC NEUTRALISATION OF THE FRMATS FOR INTERACTIONS BY USING THE PREDEFINED VECTOR COMPUTATION PRIOR TO DEALING WITH THE NEUTRALISED FORMAT:

by energy saveing and conservative , but also  a new format for usage:

a basic reference capacitator for what is ;

1) multi directional with a  non limit on the values used as the interactive emittor of relations in their full but also continual frmat as the data on a neutralisation of every external stemmic inhibitor

invertion1

File:Schuko plug and socket.png

2) the thing that can do this is basically a format of Chordis6: which means that the value basis of transparent emission by absorbance is a function of the value 6 x. This value can be used as a alternator on the vector basis to locate and multi neutralise problems by giving them a numerical value. This value then can simulate level 1 behaviour.

invertion2

3) the usage of a depth probeing to define where there are accumulations of problems on the basis of what is escapeing the environment as atmospherical data based on the responsive of a maintained positionality on the value 6=the variance of interactions as the data on the levels of vectors used in their value = x

and the background data that is not clarified to make extra mesures to locate the process in its point of extra certainments in what is a occilation by confrontative means by data computations made on the level of a 1/2 way = safe way:

by invertion 3:

inversions 1+2+3 = the reversal of data based on the functionings of the earths resources and their position in spacetime as a extra effctive motivation to continue using the formats for earth preservations while maintaining a way ahead into the processess of a 3 rd value system:

ANY VALUE B BIT (UNIVERSAL AMOUNTS) = 10 X ( 3 INVERSIONS)

A FORMAT FOR 4 INVCERTIVES IN HIGHER VELOCITY THAN THE PROBLEM OF 10 X =10Y AS A UNKNOWN 3 RD VALUE =10 Z

BY USING ADAPTATIONS OF THE INTERNALS OF ATMOSPHERICAL OCCILATIONS.

sci fi reality…..the universal bird lift process..

 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 \sigma_\mathrm{avg}\,\! 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 \tau_\mathrm{avg}\,\! is not a good approximation.

First the simple case of a prismatic bar subjected to an axial force F_\mathrm n\,\! 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 F_\mathrm n\,\! can be found. The intensity of internal forces, or stress \sigma\,\!, in the cross sectional area can then be obtained by dividing the total normal force F_\mathrm n\,\!, e.g. tensile force if acting outward to the plane or compressive force if acting inward to the plane, by the cross-sectional area A\,\! where it is acting upon. In this case the stress \sigma\,\! is a scalar quantity called engineering or nominal stress that represents an average stress (\sigma_\mathrm {avg}\,\!) over the area, i.e. the stress in the cross section is uniformly distributed. Thus, we have

\sigma_\mathrm{avg} = \frac{F_\mathrm n}{A}\approx\sigma\,\!

 

A different type of stress is obtained when transverse forces F_\mathrm\,\! 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 F_\mathrm s\,\! and in opposite direction parallel to the cross section. F_\mathrm s\,\! is called the shear force. Dividing the shear force F_\mathrm s\,\! by the area A\,\! of the cross section we obtain the shear stress. In this case the shear stress \tau\,\! is a scalar quantity representing an average shear stress (\tau_\mathrm{avg}\,\!) 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:

\tau_\mathrm{avg}= \frac{F_\mathrm s}{A}\approx\tau\,\!

 

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 m-m\,\! and n-n\,\! of the axially loaded prismatic bar. The stress on plane n-n\,\!, which is closer to the point of application of the load F\,\!, varies more across the cross section than that of plane m-m\,\!. 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 \sigma_\mathrm {avg}\,\!. 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

File:2dfdtfe.gif