Validation of nasa thermal ice protection computer codes part 3-the validation of antice

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  AI Khalil, Kannel M ^a   Horvath, Charles ^a   Miller, Dean R ^b   Wright, William B ^c  

^a Metallurgical and Mechanical Engineer   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

^c NYMA Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; CODES (SYMBOLS); ELECTRIC HEATING; HEAT FLUX; NASA; THERMOCOUPLES;

ANTI-ICING; COMPUTER CODES; ENVIRONMENTAL CONDITIONS; EXPERIMENTAL PROGRAM; ICE-PROTECTION SYSTEMS; RESEARCH CENTER; SIMULATION CODE; STEADY STATE;

ICE;

EID: 84983146617     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Miller, D.R., Bond, T.H., Sheldon, D.W., Wright, W.B., Langhals, T., AI-Khalil, K.M., Broughton, H., "Validation of NASA Thermal IceProtection Computer Codes: Part 1-Program Overview", AIM Paper 97-0049, Jan 1997.
2. Wright, W.B., AI-Khalil, K.M., Miller, D.R., "Validation of NASA Thermal Ice Protection Computer Codes: Part 2-The Validation of LEWICE/Thermal", AIAA Paper 97-0050, Jan 1997.
3. AI-Khalil, K.M., Keith, T.G., and De Witt, K.J., "Further Development of an Anti-Icing Runback Model," AIAA Paper 91-0266, Jan. 1991.
4. AI-Khalil, K.M., Keith, T.G., and De Witt, K.J., "Development of an Improved Model for Runback Water on Aircraft Surfaces," AIM Paper 92-0042, Jan. 1992.
5. Wright, W.B., "Users Manual for the Improved NASA Lewis Ice Accretion Code LEWICE 1.6", NASA CR-198355, June 1995.
6. AI-Khalil, K.M., Keith, T.G., De Witt, K.J., Nathman, J.K., Dietrich, D.A., "Thermal Analysis of Engine Inlet Anti-Icing Systems," Journal of Propulsion and Power, Vol. 6, № 5, Sept-Oct, 1990, p. 628-634.