Infrared imaging used in aerodynamic research evolved during the last 25 years into a rewarding experimental technique for investigation of body-flow viscous interactions, such as heat flux determination and boundary layer transition. The technique of infrared imaging matched well its capability to produce useful results, with the expansion of testing conditions in the entire spectrum of wind tunnels, from hypersonic high-enthalpy facilities to cryogenic transonic wind tunnels. With unique achievements credited to its past, the current trend suggests a change in attitude towards this technique: from the perception as an exotic, project-oriented tool, to the status of a routine experimental procedure
Current state of the art of numerical codes does not allow the aerodynamic and thermal design of hyp...
Current state of the art of numerical codes does not allow the aerodynamic and thermal design of hyp...
Current state of the art of numerical codes does not allow the aerodynamic and thermal design of hyp...
An experimental program was aimed at identifying areas in low speed aerodynamic research where infra...
An experimental program was aimed at identifying areas in low speed aerodynamic research where infra...
The following details recent efforts undertaken at the NASA Ames Unitary Plan wind tunnels to design...
An experimental program aimed at identifying areas in low speed aerodynamic research where infrared...
The use of infrared thermography for boundary layer detection was evaluated for use in the Cal Poly ...
The feasibility of remote in-flight boundary layer visualization via infrared in incompressible flow...
Infrared transition location estimates can be fast and useful measurements in wind tunnel and flight...
Infrared transition location estimates can be fast and useful measurements in wind tunnel and flight...
Infrared thermography has been successfully adopted in the field of flow diagnostics over the last d...
A computerized infrared (IR) scanning radiometer is employed to characterize the boundary layer deve...
A computerized infrared (IR) scanning radiometer is employed to characterize the boundary layer deve...
Current state of the art of numerical codes does not allow the aerodynamic and thermal design of hyp...
Current state of the art of numerical codes does not allow the aerodynamic and thermal design of hyp...
Current state of the art of numerical codes does not allow the aerodynamic and thermal design of hyp...
Current state of the art of numerical codes does not allow the aerodynamic and thermal design of hyp...
An experimental program was aimed at identifying areas in low speed aerodynamic research where infra...
An experimental program was aimed at identifying areas in low speed aerodynamic research where infra...
The following details recent efforts undertaken at the NASA Ames Unitary Plan wind tunnels to design...
An experimental program aimed at identifying areas in low speed aerodynamic research where infrared...
The use of infrared thermography for boundary layer detection was evaluated for use in the Cal Poly ...
The feasibility of remote in-flight boundary layer visualization via infrared in incompressible flow...
Infrared transition location estimates can be fast and useful measurements in wind tunnel and flight...
Infrared transition location estimates can be fast and useful measurements in wind tunnel and flight...
Infrared thermography has been successfully adopted in the field of flow diagnostics over the last d...
A computerized infrared (IR) scanning radiometer is employed to characterize the boundary layer deve...
A computerized infrared (IR) scanning radiometer is employed to characterize the boundary layer deve...
Current state of the art of numerical codes does not allow the aerodynamic and thermal design of hyp...
Current state of the art of numerical codes does not allow the aerodynamic and thermal design of hyp...
Current state of the art of numerical codes does not allow the aerodynamic and thermal design of hyp...
Current state of the art of numerical codes does not allow the aerodynamic and thermal design of hyp...