Thicknesses of residual ice are presented to provide information on surface contamination and associated roughness during deicing events. Data was obtained from low power ice protection systems tests conducted in the Icing Research Tunnel at NASA Lewis Research Center (LeRC) with nine different deicing systems. Results show that roughness associated with residual ice is not characterized by uniformly distributed roughness. Results also show that deicing systems require a critical mass of ice to generate a sufficient expelling force to remove the ice
Ice protection techniques have attracted significant interest, notably in aerospace and wind energy ...
Aerodynamic assessment of icing effects on swept wings is an important component of a larger effort ...
NASA, FAA, ONERA, and other partner organizations have embarked on a significant, collaborative rese...
Ice accretion codes depend on models of roughness parameters to account for the enhanced heat transf...
Tests of eight different deicing systems based on variations of three different technologies were co...
Detailed measurements of the size of roughness elements on ice accreted on models in the NASA Lewis ...
Detailed size measurements of surface roughness associated with leading edge ice accretions are pres...
Experiments were performed in the Icing Research Tunnel at NASA Glenn Research Center (GRC) to inves...
Several recent studies have been performed in the Icing Research Tunnel (IRT) at NASA Glenn Research...
Because of the significant influence of surface tension in governing the stability and breakdown of ...
Roughness on aircraft ice accretions is very important to the overall ice accretion process and to t...
When an aircraft traverses through clouds containing supercooled water droplets, in-flight icing can...
Due to numerous engine power-loss events associated with high-altitude convective weather, ice accre...
Tests were conducted on a BF Goodrich De-Icing System's Pneumatic Impulse Ice Protection (PIIP) syst...
Ice protection techniques have attracted significant interest, notably in aerospace and wind energy ...
Ice protection techniques have attracted significant interest, notably in aerospace and wind energy ...
Aerodynamic assessment of icing effects on swept wings is an important component of a larger effort ...
NASA, FAA, ONERA, and other partner organizations have embarked on a significant, collaborative rese...
Ice accretion codes depend on models of roughness parameters to account for the enhanced heat transf...
Tests of eight different deicing systems based on variations of three different technologies were co...
Detailed measurements of the size of roughness elements on ice accreted on models in the NASA Lewis ...
Detailed size measurements of surface roughness associated with leading edge ice accretions are pres...
Experiments were performed in the Icing Research Tunnel at NASA Glenn Research Center (GRC) to inves...
Several recent studies have been performed in the Icing Research Tunnel (IRT) at NASA Glenn Research...
Because of the significant influence of surface tension in governing the stability and breakdown of ...
Roughness on aircraft ice accretions is very important to the overall ice accretion process and to t...
When an aircraft traverses through clouds containing supercooled water droplets, in-flight icing can...
Due to numerous engine power-loss events associated with high-altitude convective weather, ice accre...
Tests were conducted on a BF Goodrich De-Icing System's Pneumatic Impulse Ice Protection (PIIP) syst...
Ice protection techniques have attracted significant interest, notably in aerospace and wind energy ...
Ice protection techniques have attracted significant interest, notably in aerospace and wind energy ...
Aerodynamic assessment of icing effects on swept wings is an important component of a larger effort ...
NASA, FAA, ONERA, and other partner organizations have embarked on a significant, collaborative rese...