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Recent content by laro

  1. laro

    Advance drag reduction technique

    hi, for reduction of induced drag you may want to visit www.winggrid.ch where new non-classical concepts are exposed.
  2. laro

    aerodynamic coeffcients.......

    hi, why not use for beginning what a lot of NASA people use: LINAIRPRO from Desktop Aeronautics, Inc. using simple desktop programs.
  3. laro

    Multi-element high lift wing fr steep descent

    pls check exact keystrokes for www.winggrid.ch, it will not fail to come up. the device we are working on serves primarily to reduce induced drag.
  4. laro

    Multi-element high lift wing fr steep descent

    we are working on something, that delivers consistently stall free behaviour, not necessarily at very high Cl. see www.winggrid.ch
  5. laro

    what considerations are important for designing low Re foils ?

    low Re we define as foils with Re < 150'000: case A: no microturbulence as in windtunnels. generally use flat profiles with a short section of negative pressure gradient at LE. tripping and separation avoidance devices are usually a must for Cl>0.5. e.g. Chang vortexgenerators at LE and oblique...
  6. laro

    Load Distribution on a Tapered Wing

    get connected to Desktop Aeronautics, Inc. for procurement of one of the appropriate programs. one of the best sources for classic wing designs.
  7. laro

    Wake vortex models

    hello, in our own work on wingtips at present we suggest the following categories of vortex wakes: 1. Munk-type vortex wakes; coming from wings with linear interference of spanload and trailing vortex wakes. comprising planar and non-planar wings 2. Non-Munk-types; caused by outer part of wing...
  8. laro

    High Lift non flapped airfoil wanted

    hello, in any case the actual Renolds number is very important. why? because for Re > 200'000 conventional turbulant B.L. tricks work, below we ave to use tricks curing laminar separation or recirculations. for the latter case refer to the classic book Peter Chang &quot;Flow Separation&quot;. a...
  9. laro

    how can you avoid it

    avoiding separation in positive pressure gradient is possible by injecting more kinetic energy into the boundary layer. for laminar B.L. this is far from easy and there are other tricks. see www.winggrid.ch keyword oblique grooves. this arrangement allows Cl-values up to 4 at Re down to 10'000.

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