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UH-60 Black Hawk Disturbance Rejection Study for Hover/Low Speed Handling Qualities Criteria and Turbulence ModelingThis paper will discuss the airborne flight test of the Sikorsky UH-60 Black Hawk helicopter in turbulent conditions to determine disturbance rejection criteria and develop a low speed wind/turbulence model for helicopter simulation.
Document ID
20000090530
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Labows, Steven J. (Naval Postgraduate School Monterey, CA United States)
Blanken, Chris L. (Army Aviation and Missile Command Moffett Field, CA United States)
Tischler, Mark B. (Army Aviation and Missile Command Moffett Field, CA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Aircraft Design, Testing And Performance
Funding Number(s)
PROJECT: RTOP 581-30-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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