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TELECONFRENCES
2004
The Changing Left Ventricle

2003
Aortic Valve Disease: New Dimensions in Evaluation and Management

2002
Heart Failure: Echo's Role in and Emerging Health Crisis

2001
Chest Pain in Children & Adults: The Role of Echo

2000
Mitral Regurgitation: New Concept

1998
The Falling Left Ventricle: Diastolic & Systolic Function

1997
Changing the Outcome of Coronary Artery Disease
ECHO GRAND ROUNDS
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VIDEO ARCHIVES

Chest Pain in Children and Adults

Mitral Regurgitation: New Concepts

Diastolic and Systolic Function

Changing the Outcome of CAD

BROADCAST SUPPLEMENTS
2000 MV
2001 Chest Pain
2002 Heart Failure



Estimation of the Severity of Valvular Stenosis
Estimation of the Severity of Stenosis
Fig.3.16

Use of Doppler ultrasound to estimated the severity of a valve stenosis is based principally on the fact that such obstructions result in an increase in the velocity of flow. In clinically significant mitral stenosis, the diastolic velocity of mitral flow usually exceeds 1.7 m/s. Systolic velocity of aortic flow in clinically significant aortic stenosis may reach 5-6 m/s
(Fig. 3.16). Thus, CW Doppler is required for the detection of these increased velocities and for recording the full spectral profiles.

We have already noted that there is a relationship between the pressure increase (or gradient) across a valve and the velocity of blood flow across the valve. For any given pressure gradient there is a corresponding increase in velocity, as predicted by the simplified Bernoulli equation:

p1-p2 = 4V2

where p1 = pressure distal to obstruction p2 = peak velocity of blood flow across the obstruction.

As the stenosis becomes more severe, the valve orifice area will become smaller, and the velocity of flow across the orifice will increase as a function of the increased pressure gradient. Thus, by measuring the peak velocity in a systolic aortic jet with Doppler echocardiography, it is possible to estimate the pressure gradient that produced it using the above simple algebraic expression. The peak aortic velocity of the spectral recording in Figure 3.16 is approximately 5.8 m/s. Using the previous formula

p1-p = 4(5.8)2

the pressure gradient is therefore 135 mmHg.

There are, however, three major technical requirements that must be satisfied if Doppler is to be used for this purpose. First, an adequate "window" into the chest for ultrasound propagation and reception must be found so that well formed Doppler profiles can be recorded. Second, as emphasized in Units 1 and 2, for the velocity measurement to be accurate, this window must allow orientation of the ultrasound beam so that it is as parallel as possible to flow through the valve. Third, the high velocities present in the disturbed jet often exceed the Nyquist limit of PW Doppler, so that CW or high pulse repetition frequency Doppler must be used.

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