Ice Accretion Simulation

The results of the AGARD FDP Working Group 20 on Ice Accretion Simulation are presented. This report covers the effect of ice accretion on wings, tail surfaces, engine inlets, and rotary wings. Experimentally, besides the capability of icing wind tunnel facilities, the problems of spray tanker aircr...

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Bibliographic Details
Other Authors: ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)
Format: Text
Language:English
Published: 1997
Subjects:
Snow
Ice and Permafrost
Aircraft
*ICE FORMATION
*AVIATION SAFETY
*ICE PREVENTION
NATO
FLIGHT TESTING
ICE MECHANICS
METEOROLOGICAL DATA
TANKER AIRCRAFT
WIND TUNNEL TESTS
ATMOSPHERIC PRECIPITATION
FLIGHT SIMULATION
ICE FORECASTING
AGARD(ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT)
Ice
permafrost
Online Access:http://www.dtic.mil/docs/citations/ADA336679
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA336679
Description
Summary:The results of the AGARD FDP Working Group 20 on Ice Accretion Simulation are presented. This report covers the effect of ice accretion on wings, tail surfaces, engine inlets, and rotary wings. Experimentally, besides the capability of icing wind tunnel facilities, the problems of spray tanker aircraft experiments are considered, the related similarity laws are examined, and the techniques for measuring droplet size and distribution are reviewed. The basic factors influencing computational predictions are also discussed in detail.

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