Studies conducted by Adams (1951) with respect to a body of minimum wave drag are considered, taking into account a formula describing the cross-sectional area variation for an optimum body of given length, volume, and base area for minimum wave drag. Attention is given to body shapes and questions of wave drag. The investigation shows that in a range exceeding that studied by Adams there are several optimum bodies for which the maximum area occurs at the base
The external wave drag of bodies of revolution moving at supersonic speeds can be expressed either i...
It seems possible that, in supersonic flight, unconventional arrangements of wings and bodies may of...
The problems of determining the wave drag and optimization of displacement ship lines have been cons...
Studies conducted by Adams (1951) with respect to a body of minimum wave drag are considered, taking...
By use of an approximate equation for the wave drag of slender bodies of revolution in a supersonic ...
The problem of determining the shape of slender boattail bodies of revolution for minimum wave drag ...
The problem of determining the shape of slender boattail bodies of revolution for minimum wave drag ...
The wave drag of a combination of slender bodies of revolution at zero angle of attack is studied wi...
By use of an approximate equation for the wave drag of slender bodies of revolution in a supersonic ...
Hypersonic aerodynamic performance of minimum wave drag bodies having various cross section
As an extension of the transonic area rule, a concept for interrelating the wave drags of wing-body ...
It seems possible that, in supersonic flight, unconventional arrangements of wings and bodies may of...
By means of linearized-body theory and reverse-flow theorems, the wave drag of a system of fusiform ...
The relation of Whitcomb's "area rule" to the linear formulas for wave drag at lightly supersonic sp...
The wing-body interference theory of NACA TN 2677 applied to symmetrical wings in combination with q...
The external wave drag of bodies of revolution moving at supersonic speeds can be expressed either i...
It seems possible that, in supersonic flight, unconventional arrangements of wings and bodies may of...
The problems of determining the wave drag and optimization of displacement ship lines have been cons...
Studies conducted by Adams (1951) with respect to a body of minimum wave drag are considered, taking...
By use of an approximate equation for the wave drag of slender bodies of revolution in a supersonic ...
The problem of determining the shape of slender boattail bodies of revolution for minimum wave drag ...
The problem of determining the shape of slender boattail bodies of revolution for minimum wave drag ...
The wave drag of a combination of slender bodies of revolution at zero angle of attack is studied wi...
By use of an approximate equation for the wave drag of slender bodies of revolution in a supersonic ...
Hypersonic aerodynamic performance of minimum wave drag bodies having various cross section
As an extension of the transonic area rule, a concept for interrelating the wave drags of wing-body ...
It seems possible that, in supersonic flight, unconventional arrangements of wings and bodies may of...
By means of linearized-body theory and reverse-flow theorems, the wave drag of a system of fusiform ...
The relation of Whitcomb's "area rule" to the linear formulas for wave drag at lightly supersonic sp...
The wing-body interference theory of NACA TN 2677 applied to symmetrical wings in combination with q...
The external wave drag of bodies of revolution moving at supersonic speeds can be expressed either i...
It seems possible that, in supersonic flight, unconventional arrangements of wings and bodies may of...
The problems of determining the wave drag and optimization of displacement ship lines have been cons...