Two pieces of bell artwork. I'm not sure how accurately the cutaway represents the final arrangement of the prototype aircraft as this has the earlier tail and cowling design.
There are 2 documents concerning the handling of the bell Xp-77 located in this much larger document here (be warned, its a near 100mb pdf);
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19770022115_1977022115.pdf
The relevant reports are on pages 232 and 316.
Again, the version wind tunnel tested here is pre enlarged vert stab. The reports note mostly satisfactory handling and a high rate of roll, but unsatisfactory stability with flaps deflected for landing and climb under power with flaps partially deflected, as well as instability due to sideslip in some speed regimens.
However the main thing of interest in this document is the mention of a high and low altitude version of the Xp-77, but not much info is given. Apparently the high altitude version was to have a larger diameter propeller (10.5') and a different line of thrust. Power is listed as 515 military and 450 nominal for the low altitude version with a critical alt of 12,000' and the high altitude version of approximately the same power ratings and a critical altitude of 27,000'
Given the date of the report I do not believe the high alt version described here is the improved xp-7 discussed above.
The 3-view here is from the above report because, well, it never hurts to have more 3 views!