A workable, aircraft-specific icing severity scheme

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Jeck, Richard K ^a  

^a FAA Wm J Hughes Technical Center   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRFOILS; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS;

FLIGHT TEST; ICE ACCRETION; ICING CONDITIONS; ICING INTENSITY; LIQUID WATER; OUTSIDE-AIR TEMPERATURE; POTENTIAL BENEFITS;

ICE;

EID: 84983151048     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-94     Document Type: Conference Paper

References (9)

1. Politovich, M. K., (1996): "Response of a Research Aircraft to Icing and Evaluation of Severity Indices," J. Aircraft, 33, 291-297.
2. Jeck, R., (1992): "Examination of a Numerical Icing-Severity Index," AIAA Paper 92-0164, AIAA Aerospace Sciences Meeting, Reno, Nevada, January 1992.
3. "Aeronautical Information Manual (AIM)," updated annually; Federal Aviation Administration, Washington, DC.
4. Wright, W. B., (1995): "Users Manual for the Improved NASA Lewis Ice Accretion Code LEWICE 6," Contractor Report Nfi 198355, NASA Lewis Research Center, Cleveland, OH 44135-3191. See also http://icebox. lerc. nasa. gov/LEWICE.
5. "Janes All The World's Aircraft," updated annually; See http://www. janes. com.
6. Abbott, I. H. and A. E. von Doenhoff, (1959): "Theory of Wing Sections," Dover Publications, Inc., New York, NY.
7. Selig, (1996): "UUIC Airfoil Coordinates Database; " see http://uxh. cso. uiuc. edu\-selig/ads/coord database. html.
8. Federal Aviation Regulations, in "Code of Federal Regulations, Title 14, Aeronautics and Space," updated annually; Federal Aviation Administration, Washington, DC.
9. Ludlam, F. H., (1951): "The Heat Economy of a Rimed Cylinder," Quarterly J. Roy. Met. Soc., 77, 663-666.