Seeing as the compressor is essentially unlimited aside from being a single stage centrifugal compressor, is there any chance microjets could be used to further optimize the compressor blades, volute etc, or the intake ports in the head?
https://calhoun.nps.edu/bitstream/handl ... sequence=1
"At the high Mach number case (M=0.4), the use of microjets appears to eliminate the shock structures that are responsible for triggering the shock-induced separation, establishing the fact that the use of microjets is effective even in controlling dynamic stall with a strong compressibility effect. In general, microjet jet control has an overall positive effect in terms of maintaining leading edge suction pressure and preventing flow separation."
"The laboratory results show that the microjet actuators are an effective means of controlling separation with fairly low supply pressures and flow rates. Only relatively robust and straightforward diagnostics can be used to determine the flow conditions on the UAV during flight. As such, tufts are installed on the aircraft’s wing to serve as a qualitative way of measuring control efficacy. Results from the flight tests confirm that this flow control system is capable of delaying flow separation in the complex flows occurring during flight."
https://ntrs.nasa.gov/archive/nasa/casi ... 023593.pdf
Active-Adaptive Control of Inlet Separation Using Supersonic Microjets
Microjet-based Separation Control Using a Virtual Sensor for Degree of Separation
https://static1.squarespace.com/static/ ... ontrol.pdf
Just a thought.
The height of cultivation is really nothing special. It is merely simplicity; the ability to express the utmost with the minimum. Mr.Lee