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Now showing items 1-10 of 53
On the large amplitude motion of tuned pendulum dampers
(Georgia Institute of Technology, 1960-08)
Preliminary Turboshaft Engine Design Methodology for Rotorcraft Applications
(Georgia Institute of Technology, 2006-11-20)
In the development of modern rotorcraft vehicles, many unique challenges emerge due to the highly coupled nature of individual rotorcraft design disciplines therefore, the use of an integrated product and process development ...
A method for estimating performance of single rotor helicopters
(Georgia Institute of Technology, 1958-12)
Improved testing methods for measurement of extension-twist coupling
(Georgia Institute of Technology, 1999-05)
Vertical ascent analysis of the lifting airscrew
(Georgia Institute of Technology, 1940-05)
Aeromechanical Stability Augmentation Using Semi-Active Friction-Based Lead-Lag Damper
(Georgia Institute of Technology, 2005-11-23)
Lead-lag dampers are present in most rotors to provide the required level of damping in all flight conditions. These dampers are a critical component of the rotor system, but they also represent a major source of maintenance ...
Study of the effects of rotating frame turbulence (RFT) on helicopter flight mechanics, loads, and vibration
(Georgia Institute of Technology, 1987)
Turbulence model development for rotocraft stability and control specification
(Georgia Institute of Technology, 1987)
Flight mechanics and control oriented modeling for next generation on-blade control concepts
(Georgia Institute of Technology, 2010-08-30)
A matched-harmonic confluence approach to rotor loads prediction with comprehensive application to flight test
(Georgia Institute of Technology, 2012-09-18)
Future management of helicopter fleets will be more heavily based on individual component damage tracking and less on legacy usage monitoring (flight parameter-based) methods. This enhances health assessment capabilities ...