Delta winged aircraft lose a much higher amount of speed in turns than conventional winged aircraft. Anyone know the mechanism behind this?
Found my answer. True delta winged aircraft (not the cranked delta of the F-16) experience much higher drag at higher angles of attack than conventional winged aircraft.
The wing planform of the F-16 is effectively that of a cropped delta with a 40-degree leading edge sweep.
It is also called a "cranked delta".http://www.f16falcon.com/facts/f16_5.html