Add to ORKGExploratory measurements of the mean and turbulent flow in the wall boundary layer of a 15.5- by 10.2-cm channel were obtained as part of an instrumentation development program for measurements in compressible flow. Mean surface and flow-field surveys were obtained at channel Mach numbers ranging from 0.2 to 0.9. The mean velocity distributions were obtained with total pressure probes and a laser velocimeter. At a channel Mach number of 0.2, several types of hot-wire probes were used to obtain both velocity fluctuations and Reynolds shear-stress results
January 1969Also issued as: Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanica...
The results of an experimental investigation of the mean- and fluctuating-flow properties of a compr...
Measurements of total temperature and pitot pressure across boundary layer of test section wall of a...
Experiments were carried out to test the accuracy of laser Doppler instrumentation for measurement o...
The nozzle wall boundary layer of an M-50 helium tunnel was investigated with pitot pressure, total ...
In recent years, the interest in developing a high-speed civil transport has increased. This has led...
Surveys were made through a turbulent boundary layer on a flat plate by means of a pitot probe, an x...
The development of boundary layers at high subsonic speeds in the presence of either mass flux fluct...
The turbulent boundary layer along the surface of high-speed vehicles drives shear stress and heat f...
An analysis of turbulent boundary layer flow characteristics and the computational procedure used ar...
Measurements have been made of the mean-flow and turbulence properties in adiabatic turbulent bounda...
The turbulent boundary layer along the surface of high-speed vehicles drives shear stress and heat f...
Turbulent shear stress distributions for supersonic boundary layer flows have been computed from exp...
Three mean velocity components and six Reynolds stresses were measured at two streamwise stations in...
A study was conducted to investigate development of boundary layers under the influence of velocity ...
January 1969Also issued as: Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanica...
The results of an experimental investigation of the mean- and fluctuating-flow properties of a compr...
Measurements of total temperature and pitot pressure across boundary layer of test section wall of a...
Experiments were carried out to test the accuracy of laser Doppler instrumentation for measurement o...
The nozzle wall boundary layer of an M-50 helium tunnel was investigated with pitot pressure, total ...
In recent years, the interest in developing a high-speed civil transport has increased. This has led...
Surveys were made through a turbulent boundary layer on a flat plate by means of a pitot probe, an x...
The development of boundary layers at high subsonic speeds in the presence of either mass flux fluct...
The turbulent boundary layer along the surface of high-speed vehicles drives shear stress and heat f...
An analysis of turbulent boundary layer flow characteristics and the computational procedure used ar...
Measurements have been made of the mean-flow and turbulence properties in adiabatic turbulent bounda...
The turbulent boundary layer along the surface of high-speed vehicles drives shear stress and heat f...
Turbulent shear stress distributions for supersonic boundary layer flows have been computed from exp...
Three mean velocity components and six Reynolds stresses were measured at two streamwise stations in...
A study was conducted to investigate development of boundary layers under the influence of velocity ...
January 1969Also issued as: Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanica...
The results of an experimental investigation of the mean- and fluctuating-flow properties of a compr...
Measurements of total temperature and pitot pressure across boundary layer of test section wall of a...