Flying wing does want a vertical stabilizer bcos the design contributes a little for vertical stability of plane but gives horizontal stability.....
Flying wing design and Vertical stabilizers( or directional stability) are not much related... Because the flying wings are mainly used to attain
horizontal stability (mainly longitudinal stability in pitch axis) and stealth.... That is a tailless plane (both forward and aft) can achieve horizontal stability by flying wings....
So the main requirement of a flying wing aircraft is to attain vertical stability by some other means... Flying wing designs not use large FIN or simply FIN as it negate the advantages of flying wing like stealth, low drag etc....
the best methods used are...
1.sweepback- a little effect in vertical stability but can be used...
2.crank the wing tip sections downward with significant anhedral...
3.wash out, together with a swept-back wing planform and a suitable airfoil section.
Also for controlling yaw axis (bcos no rudder in vertical fin)
1.Split ailerons. The top surface moves up while the lower surface moves down, to create an air brake effect.
2.Spoilers.
3.Spoilerons
If former Director General DRDO or Chief Scientific Advisor to the Minister of Defence can discuss it in Aerospace forum in Sweden... Why can't we bro (provided the things seems impossible though)???