Add to ORKGStatistical analysis of pressure fluctuations in separated turbulent boundary laye
Experimental data were obtained on blade self-noise generation by strong adverse-pressure-gradient a...
Direct Numerical Simulations are used to generate a database of high-speed zero-pressure-gradient tu...
The structure of the wall pressure field beneath supersonic adiabatic turbulent boundary layers is a...
Selected band cross correlation analysis of fluctuating pressures under turbulent boundary layer flo
Spectra and space-time correlations of fluctuating pressures at wall beneath supersonic turbulent bo...
Fluctuating pressures were measured beneath a Mach 5, turbulent boundary layer on a flat plate with ...
Measurements of surface-pressure fluctuations were made at two locations on the XB-70 airplane for n...
Results are presented for an investigation of surface pressure fluctuations and response of panels u...
A DNS database of turbulent boundary layers with the freestream Mach number spanning from M∞ = 2:5 t...
The surface pressure fluctuations on a flat plate model at hypersonic Mach numbers of 5.2, 7.4 and 1...
This paper describes a statistical analysis of the wall pressure fluctuations generated at the wall ...
The turbulent boundary layer on the wall of a 9 by 7 foot wind tunnel was measured with 12 different...
Preliminary estimates of space shuttle fluctuating pressure environments were made based on analyses...
Measurements of surface pressure and wake flow fluctuations were made as part of a transonic wind tu...
Turbulent flow field around supersonic space vehicles - identification of separated flow component
Experimental data were obtained on blade self-noise generation by strong adverse-pressure-gradient a...
Direct Numerical Simulations are used to generate a database of high-speed zero-pressure-gradient tu...
The structure of the wall pressure field beneath supersonic adiabatic turbulent boundary layers is a...
Selected band cross correlation analysis of fluctuating pressures under turbulent boundary layer flo
Spectra and space-time correlations of fluctuating pressures at wall beneath supersonic turbulent bo...
Fluctuating pressures were measured beneath a Mach 5, turbulent boundary layer on a flat plate with ...
Measurements of surface-pressure fluctuations were made at two locations on the XB-70 airplane for n...
Results are presented for an investigation of surface pressure fluctuations and response of panels u...
A DNS database of turbulent boundary layers with the freestream Mach number spanning from M∞ = 2:5 t...
The surface pressure fluctuations on a flat plate model at hypersonic Mach numbers of 5.2, 7.4 and 1...
This paper describes a statistical analysis of the wall pressure fluctuations generated at the wall ...
The turbulent boundary layer on the wall of a 9 by 7 foot wind tunnel was measured with 12 different...
Preliminary estimates of space shuttle fluctuating pressure environments were made based on analyses...
Measurements of surface pressure and wake flow fluctuations were made as part of a transonic wind tu...
Turbulent flow field around supersonic space vehicles - identification of separated flow component
Experimental data were obtained on blade self-noise generation by strong adverse-pressure-gradient a...
Direct Numerical Simulations are used to generate a database of high-speed zero-pressure-gradient tu...
The structure of the wall pressure field beneath supersonic adiabatic turbulent boundary layers is a...