In recent years the phase-change paint technique has evolved into an accepted diagnostic tool in high-speed wind-tunnel testing. This report documents use of the method at the Naval Surface Weapons Center, White Oak Laboratory, to study aerodynamic interference heating on fin-body configurations. Various aspects of both the underlying theory and the experimental method are enumerated based on experience and on information from other researchers. Analytic relationships are presented which indicate how uncertainties in the various input parameters affect the uncertainty in the heat-transfer coefficient. Advantages and disadvantages of the phase-change paint method are discussed.Excerpts presented at the Tenth Navy Symposium on Aeroballistics,...
In this cumulative thesis, a time-resolved quantitative temperature-sensitive paint (TSP) measuremen...
The phase-change-coating technique was used to study the interference heating to the windward surfac...
Phase change paint tests of a Rockwell International .00593-scale space shuttle orbiter were conduct...
The phase-change-coating technique was used to study the interference heating to the windward surfac...
The general purpose of this investigation was to study the separated flow field associated with a fi...
"An experimental investigation was conducted at a test-section Mach number of 4.95 and a stagnation ...
The colour/phase change paint technique requires the determination of transient conduction character...
Model information and data from wind tunnel tests conducted on 0.04 scale 50 percent forebody models...
New facilities and test techniques afford research aerodynamicists many opportunities to investigate...
The results of a wind tunnel test program to determine aerodynamic heat transfer distributions on th...
Tests were conducted in a hypersonic wind tunnel using various truncated space shuttle orbiter confi...
The Temperature Sensitive Paint (TSP) method has the potential to measure boundary-layer transition ...
A urethane based temperature sensitive paint was employed to measure the surface temperature charact...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
In order to assess the direct influence of surface roughtness upon heat transfer andits indirect eff...
In this cumulative thesis, a time-resolved quantitative temperature-sensitive paint (TSP) measuremen...
The phase-change-coating technique was used to study the interference heating to the windward surfac...
Phase change paint tests of a Rockwell International .00593-scale space shuttle orbiter were conduct...
The phase-change-coating technique was used to study the interference heating to the windward surfac...
The general purpose of this investigation was to study the separated flow field associated with a fi...
"An experimental investigation was conducted at a test-section Mach number of 4.95 and a stagnation ...
The colour/phase change paint technique requires the determination of transient conduction character...
Model information and data from wind tunnel tests conducted on 0.04 scale 50 percent forebody models...
New facilities and test techniques afford research aerodynamicists many opportunities to investigate...
The results of a wind tunnel test program to determine aerodynamic heat transfer distributions on th...
Tests were conducted in a hypersonic wind tunnel using various truncated space shuttle orbiter confi...
The Temperature Sensitive Paint (TSP) method has the potential to measure boundary-layer transition ...
A urethane based temperature sensitive paint was employed to measure the surface temperature charact...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
In order to assess the direct influence of surface roughtness upon heat transfer andits indirect eff...
In this cumulative thesis, a time-resolved quantitative temperature-sensitive paint (TSP) measuremen...
The phase-change-coating technique was used to study the interference heating to the windward surfac...
Phase change paint tests of a Rockwell International .00593-scale space shuttle orbiter were conduct...