https://www.scipedia.com/wd/index.php?action=history&feed=atom&title=Ferlauto_et_al_2021aFerlauto et al 2021a - Revision history2026-06-09T23:31:58ZRevision history for this page on the wikiMediaWiki 1.27.0-wmf.10https://www.scipedia.com/wd/index.php?title=Ferlauto_et_al_2021a&diff=219132&oldid=prevScipediacontent: Scipediacontent moved page Draft Content 511799301 to Ferlauto et al 2021a2021-03-11T16:01:21Z<p>Scipediacontent moved page <a href="/public/Draft_Content_511799301" class="mw-redirect" title="Draft Content 511799301">Draft Content 511799301</a> to <a href="/public/Ferlauto_et_al_2021a" title="Ferlauto et al 2021a">Ferlauto et al 2021a</a></p>
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<td colspan='1' style="background-color: white; color:black; text-align: center;">Revision as of 16:01, 11 March 2021</td>
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</td></tr></table>Scipediacontenthttps://www.scipedia.com/wd/index.php?title=Ferlauto_et_al_2021a&diff=219131&oldid=prevScipediacontent: Created page with "== Abstract == The aerospike nozzle represents an interesting technology for Single-Stage-To-Orbit vehicles because of its self-adapting capability. It is possible to get thr..."2021-03-11T16:01:18Z<p>Created page with "== Abstract == The aerospike nozzle represents an interesting technology for Single-Stage-To-Orbit vehicles because of its self-adapting capability. It is possible to get thr..."</p>
<p><b>New page</b></p><div>== Abstract ==<br />
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The aerospike nozzle represents an interesting technology for Single-Stage-To-Orbit vehicles because of its self-adapting capability. It is possible to get thrust vectoring capabilities in different ways. A straightforward solution consists in applying differential throttling to multiple combustion chambers which feed the nozzle. An alternative technology, which can be used in the presence of a common combustion chamber, is represented by fluidic thrust vectoring which requires the injection of a secondary flow from a slot on the wall. In this work, the flow field in a linear aerospike nozzle is numerically investigated by means of RANS simulations and both differential throttling and shock vectoring are studied. A parametric study is performed to evaluate the potential of the two technologies.<br />
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== Full document ==<br />
<pdf>Media:Draft_Content_511799301p2064.pdf</pdf></div>Scipediacontent