V at -ve n should be 110.42 m/s as per my calculations. 97.8 m/s is at -ve 1g(n=-1) not at -n(max)
@AeroInsights-1 Жыл бұрын
Worst panelist in DRDO interview just came to have tea and biscuits, and most importantly for asking illogical question , Thanks for wrapping up interview only for have tea , worst he destroyed my only chance to be an scientist.
@piers41309 ай бұрын
Origin of gust lines should be on y axis (0 EAS) at n=1, not at Vs
@뚜비두밥-n3z3 жыл бұрын
Hi I'm korean student majoring in aerospace engineering. I found this video while watching KZbin. And I became curious. I wonder which aircraft the CFR25.341 apply to. General aviation or All aircraft including fighter and transport? And I also wander what is the defference between CFR23.333 and CFR25.341. Both of them explains a gust. Is the aircraft model different? Then what is the standard? please give me answer. And thanks for useful video!
@David-oj4lq3 жыл бұрын
FAR 23 is for lightweight aircraft, while FAR 25 is for transport aircrafts like the 320 or the 737 and so on
@뚜비두밥-n3z3 жыл бұрын
@David I see. Thank you for your answer.
@SathishT3 жыл бұрын
Dear Sir, At 24:03, the unit of a is said as 'per deg' but the formula gives the value in 'per rad'. The reasoning provided for the unit does not appear to be correct as the tan of angle should always be the same irrespective of whether the angle is in radian or degree and the tan of angle is a number without unit. Kindly check.