this below is a great read, including exhaust recovery
look at Advanced Topics and Tech Paper Download (and stuff by Paul Lamar)
Paul Lamar was a racecar wing pioneer incl work for Chapparal and Pontiac
http://www.rotaryeng.net/
@ pgfpro ?
Paul L has been imo a bit optimistic
specifically on what he seems to call dumping loss across exhaust valve
and the extent to which the Mazda Rotary could escape this
(imo no engine can escape it, even with infinitely large/infinitely fast port opening, unless there is high exhaust pressure)
the rotary engine is similar to supercharged aircraft engines ie the CR is rather low so the exhaust energy is unusually high
looking again at the energy balance figs in the Wright TC paper
in lean cruise supercharger power was relatively high and recovery low (implying poor recovery in F1 below full power)
apparently even at this very lean mixture 4.6% of the fuel's energy was lost in dissociation to CO and CH4
(1800 rpm, inherently high temperatures, and maybe the high aromatic content of Avgas causing this ?)
overall efficiency was 32.5% (about 9.5% of this from recovery) with a CR around 7
so if they had made a cruise-only engine with cruise-optimised CR 35% efficiency would be possible ?
(and some of these values seem lower than would correspond to the official BSFC figures and Wright's brochure)
interestingly, Wright seem to have run eg at CR=4 and about 32 bar bmep
Engine Compounding for Power and Efficiency (Pierce&Walsh) SAE quarterly transactions Vol 2 No 2April 1948 looks quite useful
and the Barber-Nichols turbine brochure
PL shows NACA paper saying the (basic not entrainment ?) exhaust jet propulsion effect adds 2% to power at 200 mph eg to F1
ok, we knew this
and there's a paper on Detroit Diesel turbocompounding, worth up to 5% free power and proportionate increase in efficiency
btw - somewhere PL says that car engines (for high capacity with minimal length) often skimp wrt crankshaft fillet size
so have inadequate fatigue life at constant high power/rpm eg for aviation use
that Orenda (car-type 'big-block' V8 engine for aircraft) found this, even (after ?) spending $100000+ on dies for improved crankshafts ?