The Estimation of the Loading on Swept Wings With Extending Chord Flaps at Subsonic Speeds

  • Mckie, Aerodynamics Dept, +2 authors Farnborough Sljm4fy
  • Published 1969
A methai 1s given for estlmatng lift and vortex drag increments due to pan-span, extenting chord flaps on thin, sweptback, tapered va.ngs of large aspect ratio in ~nnscd, incompressible flow. It 1s a linear theory and may be consn+aw3 as a simple extension of the R.A.E. Standard Method for calcula-?;m.g load.mgs on such wings and. retains sxnilar means of… CONTINUE READING