<div class="description">
<dl><dd>Thesis Advisor(s): Reichenbach, Roy E</dd>
<dd>"March 1968."</dd>
<dd>Description based on title screen as viewed on December 4, 2007</dd>
<dd>Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, March 1968</dd>
<dd>Includes bibliographical references (p. 36-39)</dd>
<dd>A study was conducted to determine the effects of varying the fluid properties of viscosity, surface tension, and density on liquid jet breakup, penetration, and spreading. Water, heptane, and a 58 per cent glycerin-42 per cent water mixture (by mass) were injected transversely into Mach 2.8 and 4.0 airstreams through various circular orifices located in the surface of a flat plate model. Experiments were performed with injector orifices varying in diameter from 0.0145 inches to 0.080 inches, using injectant total pressures ranging from 30 psia. to 3000 psia. Steady-state penetration and lateral spreading distances were measured from scattered light photographs, and qualitative analyses of shock waves induced by the liquid jet were made using schlieren photographs. (Author)</dd>
<dd>Mode of access: World Wide Web</dd>
<dd>System requirements: Adobe Acrobat Reader</dd>
<dd>US Navy (USN) author</dd>
<dd>dk/ original 12/4/07 upgraded</dd>
<dd>Both copies are missing per dk 12/4/07</dd></dl><br>Subjects:</div>
<div class="fn value">
Castle, Robert Wellington</div>
Internet Archive identifier