
Kitne baar bcccc
LOWKY RAGEBAIT ATPPP
Bhai 15 baar bhar chuki hu, ab tk nahi hora h bccc
kab tk karu tryyy

LOWKY RAGEBAIT ATPPP
Bhai 15 baar bhar chuki hu, ab tk nahi hora h bccc
kab tk karu tryyy
here what is cuid, idxn according to icse 10th matriculate certificate
plzzzz helpp urgenttttt hhhh🥹🙏🏿🙏🏿🙏🏿
Ppl for current affairs and news what yt channel to refer. say currently I'm on zero level for CA and news, I wanna build strong foundation for upcoming NDA ssb
mai 10th certificate se register kar rahi hu.
Sooooo 10th icse k pass certificate me cuid and idxn konsa hota hhhh
PLZZZ BATAOOOO
So I am learning ansys, and ran a basic analysis...
while I just wanted the velocity and pressure distribution on the wing along with lift and drag, but we also get this residual graph.
at every iteration it it solves the equation and gives the values of k energy omega etc.... but as a whole what does it imply... like I might be wrong asw
in this case initially the values are far n converge becoming straight line. so what exactly does it say about the wing/fluid behaviour....
So basically I'm into aeromodelling (ik very different form the subreddit, but thought could get help)
As all know that elliptical planform has the best lift distribution, and is considered ideal.
but irl we don't see many planes w elliptical planform, other than manufacturing difficulties i believe presence of fuselage drastically reduces it's performance.
So I had this doubt that if this is true then, how exactly is the aerodynamics affected and any possible solns for it
Also it's effect on other planforms....