CHORDIS EU SYSTEM laws 3,4,5,6,7

application

of geometry for flying car developement

By Henryk Szubinski

GETTING ALL OF THEESE PINS ROTATING IN THE FOLD VALUES ON A TOTAL SUM SHAPE OF 4+5+6+7 SIDES =22 SIDED OUTLINE AS THE FLYING CAR PLATFORM WHICH WILL BASICALLY ALTERNATE TO THE DIFFERENCES OF THE PINS

THE PINS ARE THE RADIAL CURVATURES ON THE OUTSIDES OF THE PLATFORM

AS SUCH THIS TYPE OF PLATFORM WILL LIFT AND SUSTAIN ANY LANDING ON ANY HEIGHT VALUE WITH ANY WEIGHT ON TOP OF IT.

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basically the 3 vector strech points will define the flow of dynamics in which the flexation values in shaded sections will alternate between the flow in motion as the basis of the flow being alternated by flexation to a lift sustainement as well as the odd flex out being the flow of dynamics for a event flex EVEN basis and the ODD 3 rd flex point = to the alternations of a uneven flexation into occilation of flow through thoose open and closed sections as flow portal opened and closed in high velocity occilations of the base pressure in the dynamic stability. This then will cause a flow forwards by pressure reduction and the lift by the basics of the pressure down and the basics of the propulsion at the tail by the flow outwards this will seperate the flow down as a totally different format of the vector down at the base and the vector out at the tail defining the shared nose flow and the tail flow as a basis for a shared vector down = vector up

by basic flexations of shared 3 levels of stretching the limits.

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