TITLE:
Compressors for Hyper-Sonic Engines —A Theoretical Study of Future Compressors for Hyper Sonic Engines
AUTHORS:
Christine Cherian
KEYWORDS:
Adiabatic Compression, Power Compressor, M-B Distribution, Riemann Geometry, Matric Tensor, High Energy Molecule Ref, Bessel Function, Efficiency of the Compressor, Poly-Entropy Efficiency
JOURNAL NAME:
Advances in Aerospace Science and Technology,
Vol.3 No.4,
December
25,
2018
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].