A Theoretical Investigation of the Aerodynamics of Slender Wing-body Combinations Exhibiting Leading-edge Separation


Book Description

A theoretical analysis is presented for calculating the normal force and center of pressure on plane wing/body combinations exhibiting leading edge separation. The mathematical model for the separated flow involves the shedding of a number of discrete vortex pairs along the wing leading edge, each pair satisfying the Kutta condition at the position of shedding. The subsequent lateral positions of these vortex filaments are calculated step by step, so that the rolling up of the vortex sheet is taken into account. Hence, the method predicts the chordwise normal-force distributions as well as the vortex sheet shapes over the configuration.







On Slender Delta Wings with Leading-edge Separation


Book Description

The computations show that leading-edge separation produces an increase in lift over that given by the Jones slender-wing theory and that the lift does not vary linearly with angle of attack. Computed pressure distributions and span loadings are presented and the theoretical lift results are compared with the results of simple force tests made at a Mach number of 1.9.
















A Theoretical Study of the Aerodynamics of Slender Cruciform-wing Arrangements and Their Wakes


Book Description

A theoretical study is made of some cruciform-wing arrangements and their wakes by means of slender-body theory. The basic ideas of this theory are reviewed and equations are developed for the pressures, loadings, and forces on slender cruciforn wings and wing-body combinations. The rolling-up of the vortex sheet behind a slender cruciform wing is considered at length and a numerical analysis is carried out using 40 vortices to calculate the wake shape at various distances behind equal-span cruciform wing at 45 degrees bank. Analytical expressions are developed for the corresponding positions of the rolled-up vortex sheets using a 4-vortex approximation to the wake, and these positions are compared with the positions of the centroids of vorticity resulting from the numerical analysis. The agreement is found to be remarkably good at all distances behind the wing.




NASA Technical Note


Book Description