airrocket said:
That is a way cool concept vehicle... got to luv it.
External compression (shock confined combustion) was studied and demonstrated in depth by Dugger of JHU/APL in 1956 and RAE in 1966 (boundry layer diverter ahead of the wedge crest and a step at the wedge crest) at M10 conditions. ISP ....heated gasified hydrogen from skin cooling (energy recovery) reached ISP of 5,000 out of the nozzle (doublewedge with discret hole and wall slot injectors) prior to combustion. External compression can also be utilized to replace aerodynamic control surfaces (negative trim drag) flaps, elevators, ailerons, rudder etc...
Agreed on way cool concept ... got to luv it - Agreed!
I think we are of like mind on hypersonic concepts - let's publish them all - and do more!
And lets actually built em and fly em!
Anyway, I am unaware of Dugger's 1956 in depth study.
I have a copy of his 1958-1961 in depth study, on ERJ (External Burning Ramjet),
EEJ (External Expansion Ramjet), and HRJ (Hypersonic Ramjet). In fact, I believe
the HRJ work led to Billig's first successful scramjet engine which was external burning
initially, but which later was converted to a cowled design.
ERJ conclusion was that it was good for cruise. In fact it could produce net thrust,
and increase airfoil lift up to 2X-3X (note - airfoil lift - think of neat possible shapes!),
greatest propulsive efficiency was with slender shapes, fuel specific impulse for cruise,
at moderate hypersonic speed, was between rockets and conventional ramjets. At higher
Mach, fuel specific impulse was better that conventional ramjet (CRJ) (but remember
CRJ is subsonic burning and at higher mach, that doesn't work so well), and ERJ is actually
supersonic burning.
However ERJ as a primary powerplant is much poorer for missions requiring acceleration.
Dugger indicated that more work needs to be done on optimizing the fuel distribution and
or using favorable pressure field interference effects.
But HRJ, what we know today as scramjet, is actually better than CRJ or ERJ.
So the point is that why would you do ERJ, except for cruise optimization or control
(as you mentioned). Unless someone had made ERJ better, which we haven't seen really
any work on that I know of, as people seem to be focusing on HRJ or scramjet.
Do you have a ref. for the RAE 1966 work?
Thanks,
Larry