Results 251 to 260 of about 80,941 (296)

ECG Challenge: Focal atrial tachycardia mimicking flutter: Diagnosis clarified by ladder diagrams. [PDF]

Indian Pacing Electrophysiol J
Sánchez-Rodriguez E, Morales-Velázquez JL, Coria Sandoval PI, Coutiño Moreno HE.   +3 more
europepmc   +1 more source

A Generalized Fisher Discriminant Analysis with Adaptive Entropic Regularization for Cross-Model Vibration State Monitoring in Wind Tunnels. [PDF]

Sensors (Basel)
Li Z, Li Z, Chen X, Lin H.
europepmc   +1 more source

Inappropriate automated implantable cardioverted defibrillator therapy despite dual chamber device and evident atrial arrhythmia- what is the mechanism? [PDF]

Indian Pacing Electrophysiol J
Shaik A, Mukherjee SS, Choudhury SK, Bera D.   +3 more
europepmc   +1 more source

Atrial Fibrillation/Flutter in Transthyretin Cardiac Amyloidosis: Prevalence, Incidence, Clinical Predictors, and Effect of Tafamidis. [PDF]

JACC Adv
Chan N, Brailovsky Y, Teruya S, Mirabal A, Weinsaft AY, De Los Santos J, Guadalupe S, Jimenez M, Helmke S, Cuomo M, Smiley D, Biviano A, Dizon J, Wan E, Yarmohammadi H, Maurer MS.   +15 more
europepmc   +1 more source

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Stall-Flutter Analysis

Journal of Aircraft, 1972
An analysis of unsteady airfoil stall and stall flutter is presented that is based on a series of approximations. Unsteady aerodynamic characteristics are related theoretically to static aerodynamic characteristics. Preliminary results show good agreement with experimental dynamic stall data.
L. ERICSSON, J. REDING
openaire   +1 more source

Coupled mode flutter analysis using flutter derivatives

Journal of Wind Engineering and Industrial Aerodynamics, 1992
Abstract The “classical” coupled bending-torsion flutter of long-span bridges, possessing 3-dimensional vibration modes, is investigated both analytically and experimentally. In the analysis, self-excited forces are defined by using the so-called flutter derivatives.
H. Tanaka, N. Yamamura, M. Tatsumi
openaire   +1 more source

Nonlinear transonic flutter analysis

Dynamics Specialists Conference, 1981
A numerical procedure is presented for predicting the static and dynamic aeroelastic characteristics of thin, clean swept wings in transonic flow. The method is based upon the simultaneous time integration of the equations governing the coupled nonlinear fluid dynamic and structural aeroelastic system.
Borland, C. J., Rizzetta, D. P.
openaire   +2 more sources