Analysis and Verification of the Icing Scaling Equations. Volume 1
The formation of ice on aircraft surfaces occurs during flight through supercooled droplets. Ice accretions on these surfaces usually degrade both aircraft performance and operational safety. For this reason, it has become important in the design and certification phases of system development to eva...
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ftdtic:ADA162226 2023-05-15T16:37:19+02:00 Analysis and Verification of the Icing Scaling Equations. Volume 1 Ruff, Gary A. ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFS TN 1985-11 text/html http://www.dtic.mil/docs/citations/ADA162226 http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA162226 en eng http://www.dtic.mil/docs/citations/ADA162226 Approved for public release; distribution is unlimited. DTIC AND NTIS Aircraft Snow Ice and Permafrost Numerical Mathematics *ICE FORMATION *SCALING FACTOR *AIRFOILS SUPERCOOLING AERODYNAMICS DROPS THERMODYNAMICS SCALE MODELS MATHEMATICAL MODELS THERMAL MODELS ICE ACCRETION Text 1985 ftdtic 2016-02-22T18:35:42Z The formation of ice on aircraft surfaces occurs during flight through supercooled droplets. Ice accretions on these surfaces usually degrade both aircraft performance and operational safety. For this reason, it has become important in the design and certification phases of system development to evaluate system performance degradation because of icing. A research program was conducted to evaluate the icing scaling requirements. The objectives of the study were (1) to evaluate the equations governing the icing process to identify proposed scaling parameters, (2) to develop a computer code to solve the various forms of the icing scaling equations, (3) to conduct tests to determine which, if any, of the proposed methods produced scale ice accretions, and (4) if an accurate set of icing scaling equations were found, to write a final computer code that could be used in icing tests. The scaling verification tests were conducted using full- and half-scale circular cylinders and full-, 1/3-, and 1/ 6-scale airfoil sections. Prepared in cooperation with Sverdrup Technology, Inc., Arnold AFS, TN. Text Ice permafrost Defense Technical Information Center: DTIC Technical Reports database |
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Open Polar |
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Defense Technical Information Center: DTIC Technical Reports database |
op_collection_id |
ftdtic |
language |
English |
topic |
Aircraft Snow Ice and Permafrost Numerical Mathematics *ICE FORMATION *SCALING FACTOR *AIRFOILS SUPERCOOLING AERODYNAMICS DROPS THERMODYNAMICS SCALE MODELS MATHEMATICAL MODELS THERMAL MODELS ICE ACCRETION |
spellingShingle |
Aircraft Snow Ice and Permafrost Numerical Mathematics *ICE FORMATION *SCALING FACTOR *AIRFOILS SUPERCOOLING AERODYNAMICS DROPS THERMODYNAMICS SCALE MODELS MATHEMATICAL MODELS THERMAL MODELS ICE ACCRETION Ruff, Gary A. Analysis and Verification of the Icing Scaling Equations. Volume 1 |
topic_facet |
Aircraft Snow Ice and Permafrost Numerical Mathematics *ICE FORMATION *SCALING FACTOR *AIRFOILS SUPERCOOLING AERODYNAMICS DROPS THERMODYNAMICS SCALE MODELS MATHEMATICAL MODELS THERMAL MODELS ICE ACCRETION |
description |
The formation of ice on aircraft surfaces occurs during flight through supercooled droplets. Ice accretions on these surfaces usually degrade both aircraft performance and operational safety. For this reason, it has become important in the design and certification phases of system development to evaluate system performance degradation because of icing. A research program was conducted to evaluate the icing scaling requirements. The objectives of the study were (1) to evaluate the equations governing the icing process to identify proposed scaling parameters, (2) to develop a computer code to solve the various forms of the icing scaling equations, (3) to conduct tests to determine which, if any, of the proposed methods produced scale ice accretions, and (4) if an accurate set of icing scaling equations were found, to write a final computer code that could be used in icing tests. The scaling verification tests were conducted using full- and half-scale circular cylinders and full-, 1/3-, and 1/ 6-scale airfoil sections. Prepared in cooperation with Sverdrup Technology, Inc., Arnold AFS, TN. |
author2 |
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFS TN |
format |
Text |
author |
Ruff, Gary A. |
author_facet |
Ruff, Gary A. |
author_sort |
Ruff, Gary A. |
title |
Analysis and Verification of the Icing Scaling Equations. Volume 1 |
title_short |
Analysis and Verification of the Icing Scaling Equations. Volume 1 |
title_full |
Analysis and Verification of the Icing Scaling Equations. Volume 1 |
title_fullStr |
Analysis and Verification of the Icing Scaling Equations. Volume 1 |
title_full_unstemmed |
Analysis and Verification of the Icing Scaling Equations. Volume 1 |
title_sort |
analysis and verification of the icing scaling equations. volume 1 |
publishDate |
1985 |
url |
http://www.dtic.mil/docs/citations/ADA162226 http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA162226 |
genre |
Ice permafrost |
genre_facet |
Ice permafrost |
op_source |
DTIC AND NTIS |
op_relation |
http://www.dtic.mil/docs/citations/ADA162226 |
op_rights |
Approved for public release; distribution is unlimited. |
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1766027604669759488 |