Icing testing of a large full-scale inlet at the Arnold Engineering Development Center
Author:
Affiliation:
1. Sverdrup Technology, Inc., Arnold AFB, TN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-299
Reference11 articles.
1. The AEDC altitude testing capabilities include simulation of atmospheric supercooled water icing conditions. Tests have been conducted on one inlet of a dual-inlet nacelle of the 8-18 aircraft. The inlet was tested in the ETF propulsion development test cell J-2 in the free-jet mode. A 65-in. diam free-jet nozzle was installed to direct the simulated icing conditions to the inlet. An engine simulator controlled inlet capture ratio. The engine simulator was equipped with an engine front frame and a Herschel
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1. Simulations of Turbulent Droplet Dispersion in Wind-Tunnel Icing Clouds;Journal of Aircraft;1997-03
2. Computations of turbulent droplet dispersion for wind tunnel icing tests;34th Aerospace Sciences Meeting and Exhibit;1996-01-15
3. Turbine Engine Icing Spray Bar Design Issues;Journal of Engineering for Gas Turbines and Power;1995-07-01
4. Icing test capabilities in the Aeropropulsion System Test Facility at the Arnold Engineering Development Center;25th Plasmadynamics and Lasers Conference;1994-06-20
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