Add to ORKGA Mathematical theory is developed to perform the calculations necessary to determine the wave drag for slender bodies of non-circular cross section. The derivations presented in this report are based on extensions to supersonic linearized small perturbation theory. A numerical scheme is presented utilizing Fourier decomposition to compute the pressure coefficient on and about a slender body of arbitrary cross section
A numerical method based on the conservation form of the full potential equation has been applied to...
Method permits analysis of noncircular bodies and calculation of wing-body interference effects in p...
A computer program developed for determining the subsonic pressure, force, and moment coefficients f...
A vector study of the partial-differential equation of steady linearized supersonic flow is presente...
Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow a...
A mathematical method for determining the flow field about power-law bodies in hypersonic flow condi...
By means of linearized-body theory and reverse-flow theorems, the wave drag of a system of fusiform ...
Two different singularity methods have been utilized to calculate the potential flow past a three di...
The linear lifting surface theory which predicts the life in supersonic flow, even though the drag i...
The problem of inviscid, steady transonic conical flow, formulated in terms of the small disturbance...
Solving exact gas dynamic equations for supersonic flows far from axis of slender lifting bodie
Estimated supersonic flow field shock waves and sonic boom effects for cones and axisymmetric bodie
Linearized characteristics method, and equivalent body method for predicting flow field about axisym...
The local linearization method for axisymmetric flow is combined with the transonic equivalence rule...
Supersonic linearized conical-flow theory is used to determine the flow over slender pointed cones h...
A numerical method based on the conservation form of the full potential equation has been applied to...
Method permits analysis of noncircular bodies and calculation of wing-body interference effects in p...
A computer program developed for determining the subsonic pressure, force, and moment coefficients f...
A vector study of the partial-differential equation of steady linearized supersonic flow is presente...
Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow a...
A mathematical method for determining the flow field about power-law bodies in hypersonic flow condi...
By means of linearized-body theory and reverse-flow theorems, the wave drag of a system of fusiform ...
Two different singularity methods have been utilized to calculate the potential flow past a three di...
The linear lifting surface theory which predicts the life in supersonic flow, even though the drag i...
The problem of inviscid, steady transonic conical flow, formulated in terms of the small disturbance...
Solving exact gas dynamic equations for supersonic flows far from axis of slender lifting bodie
Estimated supersonic flow field shock waves and sonic boom effects for cones and axisymmetric bodie
Linearized characteristics method, and equivalent body method for predicting flow field about axisym...
The local linearization method for axisymmetric flow is combined with the transonic equivalence rule...
Supersonic linearized conical-flow theory is used to determine the flow over slender pointed cones h...
A numerical method based on the conservation form of the full potential equation has been applied to...
Method permits analysis of noncircular bodies and calculation of wing-body interference effects in p...
A computer program developed for determining the subsonic pressure, force, and moment coefficients f...