<div class="description">
<dl><dd>Title from cover</dd>
<dd>"Prepared for: Naval Air Propulsion Test Center"--Cover</dd>
<dd>"October 1975"--Cover</dd>
<dd>"NPS-57Nt75101"--Cover</dd>
<dd>Author(s) subject terms: Turbojet test cell, augmenter, flow model</dd>
<dd>Includes bibliographical references (p. 81)</dd>
<dd>Technical report; 1975</dd>
<dd>A two-dimensional elliptic computer model was adapted to the solution of the flow field in a turbojet thest cell section which contained the engine exhaust duct and augmenter tube. Various engine power settings, augmentation ratios, and augmenter geometries were investigated. Flow visualization and static pressure recovery were primary objectives subject to specified engine power settings and augmentation ratios. Capabilities and limitations of the model are discussed</dd></dl><br>Subjects: BOUNDARY LAYER (METEOROLOGY); OCEAN-ATMOSPHERE INTERACTION.; HURRICANES.</div>
<div class="fn value">
Hayes, Jack Douglas.;Netzer, David Willis, 1939</div>
Internet Archive identifier