Again it is pointed out that the theory assumes a leading-edge stall, and Reference 1 suggests that aquot;it may well be easier to predict ... is characterized by highly localized blowing effects near inboard-located engines in a wing configuration that has highly loaded inboard sections. ... There is therefore a conflicting design problem, since the initial design effort is directed towards preventing prematureanbsp;...
|Title||:||Fluid Dynamics of Aircraft Stalling|
|Author||:||North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel|