Full-Scale Wind Tunnel Test Of A UH-60 Individual Blade Control System For Performance Improvement And Vibration, Loads, And Noise Control
- Presented at Forum 65
- 20 pages
- SKU # : 65_2009_Norman
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Full-Scale Wind Tunnel Test Of A UH-60 Individual Blade Control System For Performance Improvement And Vibration, Loads, And Noise Control
Authors / Details: Thomas R. Norman and Colin Theodore, NASA Ames Research Center; Patrick Shinoda, U.S. Army; Daniel Fuerst and Uwe T. P. Arnold, ZF Luftfahrttechnik GmbH; Stephen Makinen, Peter Lorber, and John O’Neill, Sikorsky Aircraft CorporationRecently Viewed Items
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