Flow separation from a flat plate ahead of two blunt two-dimensional bodies was investigated in detail at Mach number 2.0. Interferograms were obtained for the separated regions, and the pitot-pressure distribution and flow directions were surveyed in one of the regions. Mach numbers calculated from density and pitot-pressure data were generally less than 0.5 in the reverse-flow regions near the plate * surface. A flow-direction survey for a model with separation at the leading edge of the flat plate showed a reverse-flow component in about half the separated region. Static pressures along the plate surface and over the blunt body were sensitive to small disturbances and small changes in stream conditions
Interferometer measurements are given of the flow fields near two-dimensional wedge and circular-arc...
A wind-tunnel investigation of an attached inflatable decelerator concept was conducicd at a Mach nu...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
An experimental investigation of separated boundary-layer flow was conducted on a two-dimensional fl...
A turbulent boundary layer separated by a forward-facing step was observed on the cylindrical portio...
Experimental measurements of mean flow properties over the leeward surface and in the near wake of a...
This document has been approved for public release and sale; its distribution is unlimited
This experimental study documents the development and separation of a hypersonic boundary layer prod...
Supersonic flow against blunt bodies placed in boundary layers or wakes is discussed qualitatively, ...
Experimental studies on the measurement of pressure fields in the region of separating and reattachi...
Interferometer measurements are given of the flow fields near two-dimensional wedge and circular-arc...
The pressure distribution and drag were determined for a spherical-nosed axially symmetric body with...
Previous experimental investigations of shock boundary layer interactions on a flat plate at free st...
An experimental and theoretical study has been made of the two-dimensional transonic flow past a 12°...
Surface pressure distributions are presented for regions where three-dimensional separated flow effe...
Interferometer measurements are given of the flow fields near two-dimensional wedge and circular-arc...
A wind-tunnel investigation of an attached inflatable decelerator concept was conducicd at a Mach nu...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
An experimental investigation of separated boundary-layer flow was conducted on a two-dimensional fl...
A turbulent boundary layer separated by a forward-facing step was observed on the cylindrical portio...
Experimental measurements of mean flow properties over the leeward surface and in the near wake of a...
This document has been approved for public release and sale; its distribution is unlimited
This experimental study documents the development and separation of a hypersonic boundary layer prod...
Supersonic flow against blunt bodies placed in boundary layers or wakes is discussed qualitatively, ...
Experimental studies on the measurement of pressure fields in the region of separating and reattachi...
Interferometer measurements are given of the flow fields near two-dimensional wedge and circular-arc...
The pressure distribution and drag were determined for a spherical-nosed axially symmetric body with...
Previous experimental investigations of shock boundary layer interactions on a flat plate at free st...
An experimental and theoretical study has been made of the two-dimensional transonic flow past a 12°...
Surface pressure distributions are presented for regions where three-dimensional separated flow effe...
Interferometer measurements are given of the flow fields near two-dimensional wedge and circular-arc...
A wind-tunnel investigation of an attached inflatable decelerator concept was conducicd at a Mach nu...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...