Hi Pasolati,
>The article has other hilarious gems as well.
Hm, I seem to have missed that article. Could you please re-post the link? :-)
>What ever Gersdorff may say, turbocharging is far more efficient than mechanical supercharger plus exhaust thrust.
Von Gersdorff quotes the DVL studies by von der Nüll, including a diagram comparing turbo-supercharged and jet-exhaust equipped engines in motive power and fuel consumption at 6 km and 12 km altitude.
At 6 km, the turbo-supercharger is more effective at about 400 km/h TAS and slower, and more efficient at at speeds up to 500 - 600 km/h TAS.
At 12 km, the turbo-supercharger is more efficient at any speed, and more effective at speeds up to 900 km/h TAS at least :-)
According to von Gersdorff, the main reason why German manufacturers didn't come up with a series production turbo-supercharger was the problem of creating high-temperature, high-speed turbines with the materials available to war-time Germany.
Additionally, most German engineers who had specialized in turbine development were employed in jet engine development, leaving turbo-supercharger development a bit under-staffed. (Insufficient engineering capacity was a major problem in all branches of the German aviation industry.)
>It is interesting to note that the advocates of the exhaust thust theory usually come from countries and manufacturers who failed to develop workable turbochargers.
Well, the contribution of exhaust thrust to total motive power often is forgotten (or at least underestimated), but the German aviation industry definitely appreciated the advantages of the turbo-supercharger - BMW, Daimler-Benz and Hirth-DVL were seriously trying to get them into series production.
(Junkers actually had them in production, but only for the Jumo 205/207 Diesel engines which were running with a relatively cool exhaust so the materials weren't a serious problem.)
Regards,
Henning (HoHun)