A study of large droplet ice accretions in the NASA-LEWIS IRT at near-freezing conditions

34th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1996, Pages

  Miller, Dean R ^a   Addy, Harold E ^a   Ide, Robert F ^b  

^a NASA GLENN RESEARCH CENTER   (United States)

^b U S ARMY RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; DROPS; NASA; TEMPERATURE;

DROPLET SIZES; EFFECT OF TEMPERATURE; FREEZING CONDITIONS; ICE ACCRETION; NATURAL ICING; REALISTIC SIMULATION; WATER DROPLETS; WATER TEMPERATURES;

ICE;

EID: 84962176120     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Performance of the Forward Scattering Spectrometer Probe in NASA's Icing Research Tunnel, Hovenac, E.,and Ide, R, NASA TM101381, AIAA- 89-0769.
2. Baumgardner, D., Corrections for the response time of particle measuring probes. Reprints of the 6th Symposium on Meteorological Observation and Instrumentation, New Orleans, January 12-16, 1987, pp. 148-151.
3. Wilbanks, C., and Schulz, R., Analytical Study of Icing Simulation for Turbine Engines in Altitude Test Cells, AEDC-TR-73-144, November 1973.
4. Jeck, R., Representative Values of Icing Related Variables Aloft in Freezing Rain and Freezing Drizzle, FAA Tech Note DOT/FAA/AR-TN95/119.
5. Shin, J. and Bond T. H., "Repeatability of Ice Shapes in the NASA Lewis Icing Research Tunnel," Journal of Aircraft, Vol 31, No. 5, pp. 1057-1063, Sept-Oct, 1994.