Add to ORKGEstimating method for lift interference of wing- body combinations at supersonic speeds
The paper describes a method for estimating the wing-body interference factor, Kw, for slender confi...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
The paper describes a method for estimating the wing-body interference factor, Kw, for slender confi...
Force and pressure distribution studies to high angles of attack on all-movable triangular and recta...
Estimating method for lift interference of wing- body combinations at supersonic speed
A method for calculating the aerodynamic loading on a wing in combination with a body is presented. ...
A method of interference is described in the present report which promises profitable application in...
Numerical method for evaluation and utilization of supersonic nacelle-wing interferenc
Prepared at Langley Research Center.N69-19641.Includes bibliographical references (p. 13).Mode of ac...
The paper describes a method for estimating the wing-body interference factor, Kw, for slender confi...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
The paper describes a method for estimating the wing-body interference factor, Kw, for slender confi...
Force and pressure distribution studies to high angles of attack on all-movable triangular and recta...
Estimating method for lift interference of wing- body combinations at supersonic speed
A method for calculating the aerodynamic loading on a wing in combination with a body is presented. ...
A method of interference is described in the present report which promises profitable application in...
Numerical method for evaluation and utilization of supersonic nacelle-wing interferenc
Prepared at Langley Research Center.N69-19641.Includes bibliographical references (p. 13).Mode of ac...
The paper describes a method for estimating the wing-body interference factor, Kw, for slender confi...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
The paper describes a method for estimating the wing-body interference factor, Kw, for slender confi...