Boundary layer developments have been measured for the flow downstream of an expansion corner when the boundary layer is disturbed by a shock wave striking the surface near the corner. It is found that most velocity profiles ...
Wind-tunnel tests have been made on a series of cambered slender wings of modified gothic planform. The main purpose of these tests was to investigate camber designs which have low lift-dependent drag and a given ...
Tests have been made at supersonic speeds up to M=2.0 on a thick cambered gothic wing of aspect ratio 0.75, together with tests on the uncambered wing of the same plan-form and thickness. The camber was designed to give ...
An investigation has been made of the properties of turbulent boundary layers in negligible pressure gradient with homogeneous injection of carbon dioxide through a porous surface. Experiments were carried out at Mach ...
Summary. This report gives further experimental results for compressible turbulent boundary layers with air injection. The experimental arrangement is similar to that used by Jeromin (R. & M. 3526) but, by a slight ...
The wind-tunnel tests on cambered gothic wings reported in Reports and Memoranda No. 3211 have been extended to include the effects of changes in design lift coefficient and of changes in spanwise camber without changes ...
An extension of slender-wing theory, introduced by Adams and Sears, has been applied to some problems concerned with the properties of slender, lifting, wings with curved leading edges at supersonic speeds. Two particular ...
The boundary-layer equations are derived for a very general co-ordinate system, and various theorems hitherto only proved in more restrictive systems are extended to this general system. The particular case of streamlines ...