<div class="description">
<dl><dd>"NPS-69-86-005"--Cover</dd>
<dd>Cover title</dd>
<dd>"Contractor report"--Cover</dd>
<dd>"Prepared for: Naval Postgraduate School, Monterey, California 93943."</dd>
<dd>"July, 1986"--Cover</dd>
<dd>Includes bibliographical references (p. 26)</dd>
<dd>Technical report; 1986</dd>
<dd>The report presents heat transfer modeling of Thrust Vector control systems using the PHOENICS computer code. Simple two-dimensional wedge and blunt bodies have been examined in supersonic cold flow, for both laminar and turbulent flow cases. The research presents a numerical solution of the supersonic compressible viscous two-dimensional flow field. Post calculations were done to estimate skin friction coefficient, surface heat flux, heat transfer coefficient and Stanton number distributions in both wedge and blunt cases</dd></dl><br>Subjects: PROJECTILES--TESTING.; DRAG (AERODYNAMICS)--MEASUREMENTS.; ROTATIONAL MOTION (RIGID DYNAMICS); WIND TUNNELS.</div>
<div class="fn value">
Leitner, A. (Amiram).</div>
Internet Archive identifier