Add to ORKGAll calculations were done in the stability axes system. The winglets used were constructed of modified GA(w)-2 airfoils. Aerodynamic characteristics discussed include: angle of attack; lift-curve slope; side force; yawing moments; rolling moments
An analytical method is presented for predicting lateral-directional aerodynamic characteristics of ...
A method is presented for calculating the shape sensitivity of a wing aeroelastic response with resp...
A family of three Close Air Support aircraft is presented. These aircraft are designed with commonal...
The static and dynamic characteristics of seven helicopter sections and a fixed-wing supercritical a...
The trajectories of the wing tip vortices of a typical agricultural aircraft were experimentally det...
An analysis is made of the stability of an airplane with ailerons free, with particular attention to...
The final design of a hypersonic, SCRAMjet research aircraft, which is to be dropped from a carrier ...
Studies of transport aircraft designed for boom-free supersonic flight show the variable sweep obliq...
The curved flow capability of a stability wind tunnel was used to investigate the lateral directiona...
An experimental investigation was conducted to determine the effects of surface finish, fillet radiu...
Trailing vortices generated by lifting surfaces such as helicopter rotor blades, ship propellers, fi...
A theory is developed, for the inviscid, incompressible flow past a thin airfoil equipped with a thi...
Experiments similar to those carried out with the A.E.G (Allgemeine Elektrizitats-Gesellschaft) were...
High-lift system aerodynamics has been gaining attention in recent years. In an effort to improve ai...
Experimental crosswire measurements of the flowfield above a 70 and 75 degree flat plate delta wing ...
An analytical method is presented for predicting lateral-directional aerodynamic characteristics of ...
A method is presented for calculating the shape sensitivity of a wing aeroelastic response with resp...
A family of three Close Air Support aircraft is presented. These aircraft are designed with commonal...
The static and dynamic characteristics of seven helicopter sections and a fixed-wing supercritical a...
The trajectories of the wing tip vortices of a typical agricultural aircraft were experimentally det...
An analysis is made of the stability of an airplane with ailerons free, with particular attention to...
The final design of a hypersonic, SCRAMjet research aircraft, which is to be dropped from a carrier ...
Studies of transport aircraft designed for boom-free supersonic flight show the variable sweep obliq...
The curved flow capability of a stability wind tunnel was used to investigate the lateral directiona...
An experimental investigation was conducted to determine the effects of surface finish, fillet radiu...
Trailing vortices generated by lifting surfaces such as helicopter rotor blades, ship propellers, fi...
A theory is developed, for the inviscid, incompressible flow past a thin airfoil equipped with a thi...
Experiments similar to those carried out with the A.E.G (Allgemeine Elektrizitats-Gesellschaft) were...
High-lift system aerodynamics has been gaining attention in recent years. In an effort to improve ai...
Experimental crosswire measurements of the flowfield above a 70 and 75 degree flat plate delta wing ...
An analytical method is presented for predicting lateral-directional aerodynamic characteristics of ...
A method is presented for calculating the shape sensitivity of a wing aeroelastic response with resp...
A family of three Close Air Support aircraft is presented. These aircraft are designed with commonal...