Zobrazeno 1 - 10
of 39
pro vyhledávání: '"Lance Richards"'
Autor:
Lance Richards, Jocelyn S. Thompson, Christopher E. Knoepke, Peter M. Buttrick, David J. Magid, Grace Venechuk, Tristan J. Dow, James R. Strader, Kenneth Pierce, Robert L. Page, David P. Kao, Katy E. Trinkley, Geoffrey Harger, Larry A. Allen, Daniel D. Matlock, Pamela N. Peterson, Laura Helmkamp, Janice Huang, Colleen K. McIlvennan, Prateeti Khazanie
Publikováno v:
Circulation
Background: Major gaps exist in the routine initiation and dose up-titration of guideline-directed medical therapies (GDMT) for patients with heart failure with reduced ejection fraction. Without novel approaches to improve prescribing, the cumulativ
Publikováno v:
In Optical Fiber Technology May 2012 18(3):157-160
Publikováno v:
Aerospace, Vol 3, Iss 3, p 18 (2016)
Technological advances have enabled the development of a number of optical fiber sensing methods over the last few years. The most prevalent optical technique involves the use of fiber Bragg grating (FBG) sensors. These small, lightweight sensors hav
Externí odkaz:
https://doaj.org/article/e6da683ab0454efd98a401cb74ce3947
Autor:
Jocelyn S. Thompson, Lance Richards, Christopher E. Knoepke, Pamela N. Peterson, Grace Venechuk, James R. Strader, Katy E. Trinkley, Janice Huang, David P. Kao, Laura Helmkamp, Colleen K. McIlvennan, Prateeti Khazanie, Kenneth Pierce, Peter M. Buttrick, Larry A. Allen, Robert L. Page, Tristan J. Dow, David J. Magid, Daniel D. Matlock
Publikováno v:
American heart journal. 229
Background Heart failure with reduced ejection fraction (HFrEF) benefits from initiation and intensification of multiple pharmacotherapies. Unfortunately, there are major gaps in the routine use of these drugs. Without novel approaches to improve pre
Autor:
Eric L. Christiansen, Francisco Pena, Anthony Piazza, Allen R. Parker, W. Lance Richards, Steven L. Rickman
Publikováno v:
Procedia Engineering. 188:233-240
Spacecraft in low earth orbit (LEO) experience a variety of hazards including exposure to micrometeoroids and orbital debris (MMOD). Average impact speeds for orbital debris on spacecraft in LEO are 9 to 10 km/s, and 20 km/s for micrometeoroids. Due
Autor:
David J. Magid, Jocelyn S. Thompson, Colleen K. McIlvennan, Prateeti Khazanie, David P. Kao, Pamela N. Peterson, Janice Huang, James R. Strader, Grace Venechuk, Laura Helmkamp, Daniel D. Matlock, Katy E. Trinkley, Robert L. Page, Peter M. Buttrick, Lance Richards, Christopher E. Knoepke, Tristan J. Dow, Kenneth Pierce, Larry A. Allen
Publikováno v:
Journal of Cardiac Failure. 26:S69
Introduction Guideline Directed Medical Therapy (GDMT) recommends a combined regimen of beta blockers, ACE-I/ARB/ARNI, and mineralocorticoid receptor agents for optimal treatment of patients with Heart Failure with Reduced Ejection Fraction (HFrEF).
Autor:
Allen R. Parker, Francisco Pena, W. Lance Richards, Nathaniel W. Gardner, Michelle T. Rudd, Anthony Piazza, Mark W. Hilburger, Marc R. Schultz
Publikováno v:
2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The National Aeronautics and Space Administration (NASA) Engineering and Safety Center Shell Buckling Knockdown Factor Project is a multicenter project tasked with developing new analysis-based shell buckling design guidelines and design factors (i.e
Publikováno v:
26th International Conference on Optical Fiber Sensors.
Over the past century aircraft wing design has transformed from the morphing wing used on the Wright Flyer to rigid wings with little to no shape-tailoring abilities. Modern day wings are designed to fly at a single trim condition and optimized to ha
Autor:
John A. Bakalyar, Helen Boussalis, Sami F. Masri, Armen Derkevorkian, W. Lance Richards, Jessica Alvarenga
Publikováno v:
AIAA Journal. 51:2231-2240
A new deformation shape-sensing methodology is investigated for the purposes of real-time condition assessment, control, and health monitoring of flexible lightweight aerospace structures. The fiber optic strain sensing technology was recently propos
Publikováno v:
Key Engineering Materials. 558:268-280
The thermal protection systems of spacecraft are vulnerable to damage from impacts by foreign objects moving at high velocities. This paper describes a proposed novel structural health monitoring system that will detect, locate and evaluate the damag