bobbymike said:
LowObservable said:
That would be a remarkable feat of aerodynamic and propulsive technology. Consider the fact that you're going M=1.2 with one wing swept 62 deg and the other swept 22 deg. Consider the cross-sectional area that the body presents to the airflow and what the shock off the nose looks like. Consider the side loads on the vertical tails and the fact that one H-tail is now washed by turbulent flow in the wake of the body. Consider the asymmetric conditions at the engine inlets.
I call shenanigans.
Not a perfect comparison as you're turning the whole plane but I think aerodynamically it could be done for short periods of flight for sensor alignment as TomS wrote.
I appreciate the fact that you mentioned that this may be an imperfect comparison. That being said, i will pitch in my .02.
This is too much of apples and oranges, me thinks. In the case of the AD-1, there is virtually no shift in the center of lift, nothing really to generate yaw moments since the fuselage remains straight and whatever asymmetric yaw the forward swept side vs. the rearward swept side generates is small.
Notice that there are no oblique wings that are not also straight, so planform geometry matters to make it viable.
Also i doubt it ever flew at anything above 200 KTAS.
The closest thing i can think of was F-16 AFTI, but you need some sort of force effector (aerodynamic surface, thrust vectoring) in order to cancel any moments and keep the vehicle aligned in the desired orientation.