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