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INTERACTIVE ANALYSIS AND DISPLAY SYSTEM (IADS) TO SUPPORT LOADS/FLUTTER TESTINGWilliams, Jenny, Lange, Don, Mattingly, Pat, Suszek, Eileen 10 1900 (has links)
International Telemetering Conference Proceedings / October 25-28, 1999 / Riviera Hotel and Convention Center, Las Vegas, Nevada / The Interactive Analysis and Display System (IADS) provides the structures flight test
engineer with enhanced test-data processing, management and display capabilities
necessary to perform safety critical aircraft analysis in near real-time during a flight test
mission. The IADS provides enhanced situational awareness through an analysis and
display capability designed to increase the confidence of the engineer in making clearance
decisions within the Mission control Room (MCR) environment. The engineer achieves
this confidence level through IADS’ real-time display capability and simultaneous near
real-time processing capability consisting of both time domain and frequency domain
analyses. The system displays real-time data while performing interactive and automated
near real-time analyses; alerting the engineer when displayed parameters exceed
predefined threshold limits. Real-time data and results created in near real-time may be
compared to previous flight test data to enhance the user’s confidence in making point-to-point
clearance decisions.
The IADS provides a post flight capability at the engineer’s project area desktop, with a
user interface common with the real-time system. The post flight IADS provides all of the
capabilities of the real-time IADS with additional data access and data organization,
allowing the engineer to perform structural analysis with test data from the each flight and
compile summary plots and tables over the most of the test program. The IADS promotes
teamwork by allowing the engineers to share data and test results during a mission and in
the post flight environment. This paper discusses the system overview and capabilities of
the IADS.
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The prevalence of atrial fibrillation in the UK and of suitability for warfarin treatment amongst those with atrial fibrillationSudlow, Christopher Mark January 1999 (has links)
No description available.
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Flutter of cylindrical shells conveying fluid.Denise, Jean-Paul François. January 1971 (has links)
No description available.
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Flutter analysis of open-truss stiffened suspension bridges using synthesized aerodynamic derivativesAl-Assaf, Adel, January 2006 (has links) (PDF)
Thesis (Ph. D.)--Washington State University, December 2006. / Includes bibliographical references (p. 148-156).
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The effect of pilot restraint and aerodynamic forces on the flutter of reversible control systems /Murphy, John Allen, January 1970 (has links)
Thesis (Ph. D.)--Ohio State University, 1970. / Includes bibliographical references (leaves 72-73). Available online via OhioLINK's ETD Center.
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Flutter of cylindrical shells conveying fluid.Denise, Jean-Paul François. January 1971 (has links)
No description available.
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Effect of compressibility on three-dimensional helicopter rotor blade flutterWhite, William Felton 05 1900 (has links)
No description available.
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Flutter suppression of an unswept wing using acceleration feedback controlLim, Mun Hong 08 1900 (has links)
No description available.
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Helicopter blade-tip stability in forward flightShipman, Keith Waldo 08 1900 (has links)
No description available.
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A 3D Theodorsen-based rotor blade flutter model using normal modes /Rauchenstein, Werner J. January 2002 (has links) (PDF)
Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, September 2002. / Thesis advisor(s): E. Roberts Wood, Mark A. Couch. Includes bibliographical references (p. 55-56). Also available online.
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