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Factors affectong Cl-2 (in Hindi)
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Cl

Priya Malani
Hello! BTech(Aerospace),Cleared Afcat(2 times),Cry Volunteer,Stem Education Enthusiast.

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sir quantitative aptitude course agane join cheyanam
  1. FACTORS AFFECTING CI By Priya Malani


  2. Bachelors in Technology in Aerospace SRM UNIVERSITY Cleared AFCAT II-2017 Cleared AFCAT I-2018 Gate Aspirant ABOUT ME 2 Educator on Unacademy


  3. HELLO I am Priya Malani I am here because I love to share my knowledge.You can find me at @https://unacademy.com/user/priy amalani96-4980 7 unacademy


  4. FACTORS AFFECTING CI By Priya Malani


  5. CI The AOA of the mainplane The wing shape both cross-section & planform The airfoil surface condition The reynolds number The local speed of sound


  6. EFFECT OF LEADING EDGE EFFECT OF WING SHAPE RADIUS EFFECT OF CAMBER EFFECT OF ASPECT RATIO EFFECT OF WING PLANFORM EFFECT OF SWEEPBACK


  7. EFFECT O LEADING EDGE RADIUS Lift is same for different leading edge radiuses up to 15 AOA. Large LE radius. large rounded peak[_slow transformation to stalled condition Beyond that the Small LE leading edge radii & the surface condition determine the stalling characteristics radius:abrupt stall


  8. Airfoils with same thickness distribution about the mean camber O EFFECT OF CAMBER line but with increasing camber shows that in Cl vs AOA, the graph line moves up & left with increasing camber. Zero lift AOA: Highly cambered wing(- 9), normally cambered(-4) & non cambered(0) Max lift at stalling angle: Highly cambered(0.88@14.5), normally


  9. Low AR wing : wing tip vortices are large & strong so, large reduction of lift EFFECT OF ASPECT RATIO High AR wing: wing vortices cause small downwash so,minimum reduction of lift


  10. 10 "THE WING E PLANFORM'"c THE-GREATEST AMOUNTOF tifTIS, PRODUCED ( BY RECTANGULAR WING AT THE WING ROOT


  11. 12 THANKS Any questions? You can find me at @https://unacademy.com/user/ priyamalani96-4980