Airspeed to achive an equivalent of dynamic pressure increase of 1013 mB
I have put numbers in to the basic noddy formula 1/2 Roh V squared and it comes out as around 400 Metres / second 777 Knots.
(a) surely this is too high
(b) If it was close to the mark pressumably it would be useless as it is higher than mach one.
Anyone got any idea on how fast you would need to fly to double the pressure?
Thanks in advance