This presentation accompanies the paper titled Plans and Preliminary Results of Fundamental Studies of Ice Crystal Icing Physics in the NASA Propulsion Systems Laboratory. NASA is evaluating whether PSL, in addition to full-engine and motor-driven-rig tests, can be used for more fundamental ice-accretion studies that simulate the different mixed-phase icing conditions along the core flow passage of a turbo-fan engine compressor. The data from such fundamental accretion tests will be used to help develop and validate models of the accretion process. This presentation (and accompanying paper) presents data from some preliminary testing performed in May 2015 which examined how a mixed-phase cloud could be generated at PSL using evaporative coo...
NASA, FAA, ONERA, and other partner organizations have embarked on a significant, collaborative rese...
The NASA Glenn Icing Research tunnel has been using an Icing Blade technique to measure cloud liquid...
Engine Icing Performance loss: rollback, surge, flameout, and even internal engine damagePartial mel...
This presentation shows results from an initial study of the fundamental physics of ice-crystal ice ...
In 2015 the FAA added Appendix D to Part 33 engine certification requirements that included Mixed Ph...
This paper builds on previous work that compares numerical simulations of mixed-phase icing clouds w...
The Icing Research Tunnel at NASA Glenn has recently switched from using the Icing Blade to using th...
The NASA Glenn Research Center Propulsion Systems Lab (PSL) was recently upgraded to perform engine ...
Preliminary results from the heavily instrumented ALF502R-5 engine test conducted in the NASA Glenn ...
This presentation is intended for a technical audience. It describes NASA Glenn's two icing-capable ...
The Propulsion Systems Laboratory (PSL) is an existing altitude simulation jet engine test facility ...
The design and certification of modern transport airplanes for flight in icing conditions increasing...
Ice crystals found at high altitude near convective clouds are known to cause jet engine power-loss ...
The aviation industry continues to deal with icing-related incidents and accidents on a regular basi...
This paper describes plans and preliminary results for using the NASA Propulsion Systems Lab (PSL) t...
NASA, FAA, ONERA, and other partner organizations have embarked on a significant, collaborative rese...
The NASA Glenn Icing Research tunnel has been using an Icing Blade technique to measure cloud liquid...
Engine Icing Performance loss: rollback, surge, flameout, and even internal engine damagePartial mel...
This presentation shows results from an initial study of the fundamental physics of ice-crystal ice ...
In 2015 the FAA added Appendix D to Part 33 engine certification requirements that included Mixed Ph...
This paper builds on previous work that compares numerical simulations of mixed-phase icing clouds w...
The Icing Research Tunnel at NASA Glenn has recently switched from using the Icing Blade to using th...
The NASA Glenn Research Center Propulsion Systems Lab (PSL) was recently upgraded to perform engine ...
Preliminary results from the heavily instrumented ALF502R-5 engine test conducted in the NASA Glenn ...
This presentation is intended for a technical audience. It describes NASA Glenn's two icing-capable ...
The Propulsion Systems Laboratory (PSL) is an existing altitude simulation jet engine test facility ...
The design and certification of modern transport airplanes for flight in icing conditions increasing...
Ice crystals found at high altitude near convective clouds are known to cause jet engine power-loss ...
The aviation industry continues to deal with icing-related incidents and accidents on a regular basi...
This paper describes plans and preliminary results for using the NASA Propulsion Systems Lab (PSL) t...
NASA, FAA, ONERA, and other partner organizations have embarked on a significant, collaborative rese...
The NASA Glenn Icing Research tunnel has been using an Icing Blade technique to measure cloud liquid...
Engine Icing Performance loss: rollback, surge, flameout, and even internal engine damagePartial mel...