Thanks,
I do not know an angle as it is only theoretical,
but I would like to know how to calculate 90deg to the vertical i.e. directly behind the aircraft and
a 30deg below the horizontal
If an aircraft is flying straight and level and drops a load but it remains attatched to the aircraft by a cable (hung load), how do I calculate the tension in the cable. I know the aircraft speed, the weight og the load and the length of the cable.
Thanks