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Static and Dynamic Response of a Design of Differential ... - aerade

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List <strong>of</strong> Syrdmls<br />

1 Introduction<br />

2 Test ecpipent<br />

3 <strong>Static</strong> response<br />

LIST OF CONTZXTS<br />

3.1 CaMration <strong>of</strong> pressure difference variation with<br />

incidence<br />

3.2 Discrepancy between present results ana those <strong>of</strong> ref.3<br />

3.3 Resolution dth roll angle<br />

3.4 Pitot <strong>and</strong> static pressure measurements<br />

3.5 Determination <strong>of</strong> incidence, roll an&e <strong>and</strong> Mach i'ro.<br />

from flight records<br />

4 <strong>Dynamic</strong> tests<br />

5<br />

References<br />

4.r <strong>Response</strong> equation<br />

it.2 Theoretical acoustic characteristics at supersonic<br />

speeds<br />

4.3 Measurement technique<br />

4.4 Tests <strong>and</strong> resulks<br />

4.5 Ihcrepancy between the response in still <strong>and</strong><br />

sqcrsonic air<br />

4.6 Further dwelopment<br />

Conclusiolls<br />

LIST OF APEWDICES<br />

Effect <strong>of</strong> inaccurate pressure hole location<br />

Condition that 25, t3

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