So if we did this head first rocket strapped and you would keep your arms at 180 degrees at mach 1 they would be at 90 degrees or 45 degree angle each and at mach 2 30 degree from the tip of your head or going of your center bodyline 15 degrees each side
After this speed the blades needs to be in the angle and if possible the tips need to trace the maximum allowed angle the be still a aficient control surface
So if i stil may continue?...
The main fusalage is the main displacer/mass body.
It will create the mach angle (at mach 1 its around a 90 degree angle at mach 2 its around a 30 degree angle)
In most cases the rotor is mounted at the top helicopter and the blades sticking beyond the nose of...
So my question is this wat if we could keep the blades inside of the mach angle/cone created by the main fuselage some how (someting like the folding wings of a f14 tomcat) keeping the tips of the rotor blades inside the mach angle
Could we keep them spinning and use jet propulsion and stub...
Hahaha if you would crash and burn at least it would be a exiting way to go out...
What i really meant was the main fuselage is capable off that kind of speed right? Also the main fusalege is what would create the mach angle/ cone?
What happens to the rotors if they would stay inside the mach...
Next to all this, the question is what are helicopters designed for what role do they need to fill.
Supersonische flight ? No we have jets to do that.
So what then?
The function that i read about in the comments that i would think would be best is the wispher or silent mode.
Does it need to...
Then there is the question how big can we make the wings how much speed need to create enough lift.
Can we gain enough elefation to do maybe a nose dive transition to gain speed and time for the transition?
So how fast can we get this helicopter to on its rotors until the wings will create enough lift to support the transition, how big would they need to be without interfering with normal hover mode then their is how is everything going to fit in a certain mach angle
I think no one also did reasurch on mach angles created by the main fuselage and how blades would fit inside that angle/cone and as most of the blades stick past the fuselage they would be expost to even greater forces