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  • About
  • The Global ETD Search service is a free service for researchers to find electronic theses and dissertations. This service is provided by the Networked Digital Library of Theses and Dissertations.
    Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
21

INTERACTIVE ANALYSIS AND DISPLAY SYSTEM (IADS) TO SUPPORT LOADS/FLUTTER TESTING

Williams, 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.
22

The prevalence of atrial fibrillation in the UK and of suitability for warfarin treatment amongst those with atrial fibrillation

Sudlow, Christopher Mark January 1999 (has links)
No description available.
23

Flutter of cylindrical shells conveying fluid.

Denise, Jean-Paul François. January 1971 (has links)
No description available.
24

Flutter analysis of open-truss stiffened suspension bridges using synthesized aerodynamic derivatives

Al-Assaf, Adel, January 2006 (has links) (PDF)
Thesis (Ph. D.)--Washington State University, December 2006. / Includes bibliographical references (p. 148-156).
25

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.
26

Flutter of cylindrical shells conveying fluid.

Denise, Jean-Paul François. January 1971 (has links)
No description available.
27

Effect of compressibility on three-dimensional helicopter rotor blade flutter

White, William Felton 05 1900 (has links)
No description available.
28

Flutter suppression of an unswept wing using acceleration feedback control

Lim, Mun Hong 08 1900 (has links)
No description available.
29

Helicopter blade-tip stability in forward flight

Shipman, Keith Waldo 08 1900 (has links)
No description available.
30

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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