An aircraft with zero drag would be perfect in retaining energy. In that technical sense, retaining energy thus is the minimization of drag, especially induced drag since it is the larger component during maneuvers with substantial g's. I would think Spitfires would be among the best there. However, during the maneuver, the engine is also contributing energy, so if you include the effect of the engine, it is possible for a plane to go through a maneuver and have more energy at the completion of it back to the same altitude (consider a slight dive starting at 150 mph from 5000 ft to 4000 ft under full power, then back up to 5000 ft and ending up with more than 150 mph). Taking that into account, it could be that an airplane with less induced drag (a Spit I, for example) could be outdone by a plane with a more induced drag but a bigger engine that more than compensates. The La-7 does well there by Widewing's tests.