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  • 1
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    In:  CASI
    Publication Date: 2006-01-12
    Description: Icing parameters have created problems and the problem areas that still exist today are presented. The problem areas include; (1) instrumentation; (2) test facilities; (3) weather forecasting of icing conditions; (4) meteorological design criteria; and (5) meteorological data.
    Keywords: METEOROLOGY AND CLIMATOLOGY
    Type: Tenn. Univ. Space Inst. Proc. of the 2nd Ann. Workshop on Meteorol. and Environ. Inputs to Aviation Systems; p 193-199
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  • 2
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    In:  CASI
    Publication Date: 2006-01-12
    Description: A representative of the U.S. Army Research and Technology Laboratories was called upon to brief the workshop on results of flight test experiments with ice-phobic coatings applied to helicopter rotor blades. An overview of the Applied Technology Laboratory helicopter icing R and D program is presented.
    Keywords: METEOROLOGY AND CLIMATOLOGY
    Type: Tenn. Univ. Space Inst. Proc. of the 2nd Ann. Workshop on Meteorol. and Environ. Inputs to Aviation Systems; p 139-152
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  • 3
    Publication Date: 2006-01-12
    Description: Helicopter ice protection design criteria was developed and technological shortcoming in meeting helicopter mission requirements is that of helicopter rotor blade ice protection. Airframe components are protected using existing technology while the rotor blade protected using the cyclic electrothermal deicing concept.
    Keywords: AERODYNAMICS
    Type: NASA. Lewis Res. Center Aircraft Icing; p 39-65
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