Abstract
This paper is an eye opening to the new horizon of the design of operational Compressors in our jet engines. That are compressors usually perform an operation called isentropic process and which levitate the pressure and temperature to the optimum level which require for effective ignition. Basically, our compressors have several sets of blades to perform this function, more precisely saying Rotor and stator blades. Where rotor blade provides air molecule to push at very high velocity to the Stationary blade and when the air Enders to the Stator, the stator races its pressure to move on to the next stage. And we call this set of Stator and rotor as a stage ref [1]. However, in this work, I consider the geometry of the incoming air molecule and how it transforms its physical quantities such as Pressure and temperature ref [2]. For that I tie the concept of Thermodynamic and mechanics on the platform of Tensor analysis ref [3]. That is, I consider the quantities like Pressure, Temperature and rate of flow are their corresponding vector spaces and energy related quintets like heat, work as the scaling elements on the above vector space. And quantities such as entropy enthalpy and specific heat capacity are corresponding physics of it. Considering the advantages, one of the important advantages of this approach is the applicability of results of this work to the formulation of blade less compression Example: Ram and Scram jet engine. Again, the relevant upgrading which is essential for future hypersonic air crafts can achieve from this study and this will be a mile stone for bright air and space travel. To conclude, this approach will be a great transformation on the conventional idea for realization of compression for operational Scram and Ram jet engines ref [4] [5].
Highlights
In most of the time, people are looking for manufacturing new meshing for exploring the unreachable heights
In this work, I consider the geometry of the incoming air molecule and how it transforms its physical quantities such as Pressure and temperature ref [2]
To solving that we provide high ambient Temperature jest before its Enders to the compressor casing and maintain this condition in the compressor casing, by this we can create random motion of air molecule ref. [10]-[16]
Summary
In most of the time, people are looking for manufacturing new meshing for exploring the unreachable heights. We are trying to make our space dreams come true To make it real, we need an ultra-modern engine for flying our air craft in to the unending space. Scram jets travel at the speed of mac 6 and above and our traditional piles need to bring risk to control the craft and the payload. When they decrease the speed the self-compression capability of Air molecule will lose so they should maintain the ship above the speed of mac 3. Organizations like NASA ISRO ESA and Russian Space Agency are looking for the solution of this set of problems ref [6] [7] [8]
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