Application of Viscous and Inviscid Computation Methods for Rocket Turbopump Systems

This paper examines current research efforts underway at Lewis Research Center which have focused on improving the structural durability of the SSME turbodrive system through more fully examining the aerothermodynamics of the flow system. This objective was achieved by developing three-dimensional v...

Full description

Saved in:
Bibliographic Details
Main Authors: Povinelli, Louis A, Haas, Jeffrey E, MeLallin, Kerry L, Schwab, John R, Chima, Rodrick V
Format: Report
Language:English
Online Access:Request full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by
cites
container_end_page
container_issue
container_start_page
container_title
container_volume
creator Povinelli, Louis A
Haas, Jeffrey E
MeLallin, Kerry L
Schwab, John R
Chima, Rodrick V
description This paper examines current research efforts underway at Lewis Research Center which have focused on improving the structural durability of the SSME turbodrive system through more fully examining the aerothermodynamics of the flow system. This objective was achieved by developing three-dimensional viscous and inviscid computer codes to predict the pressure and temperature distributions in the engine flow passages, particularly within the SSME turbines and turnaround ducts.
doi_str_mv 10.4271/841522
format report
fullrecord <record><control><sourceid>sae_AEUUQ</sourceid><recordid>TN_cdi_sae_technicalpapers_841522</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>841522</sourcerecordid><originalsourceid>FETCH-sae_technicalpapers_8415223</originalsourceid><addsrcrecordid>eNqNjssKgkAYRocoyG7P8PcAljNeW4YUtWhT0lamcURLncF_DHr7BHuAVocPDnyHkBV1Nh4L6TbyqM_YiFgsiCLbDVg4JpZDvcgO6Y5OyQzx6Tgu9UPPIsle66oU3JSqAZXDvUShOgTeZHBu3v0qM4hVrTszOBdpCpUh5KqFqxIvaSDp2ofSXa3h9kEja1yQSc4rlMsf52R9PCTxyUYuUyNF0fSPleZatpgOue4_zhcnYkRX</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Application of Viscous and Inviscid Computation Methods for Rocket Turbopump Systems</title><source>SAE Technical Papers, Back File B (1980-1989)</source><creator>Povinelli, Louis A ; Haas, Jeffrey E ; MeLallin, Kerry L ; Schwab, John R ; Chima, Rodrick V</creator><creatorcontrib>Povinelli, Louis A ; Haas, Jeffrey E ; MeLallin, Kerry L ; Schwab, John R ; Chima, Rodrick V</creatorcontrib><description>This paper examines current research efforts underway at Lewis Research Center which have focused on improving the structural durability of the SSME turbodrive system through more fully examining the aerothermodynamics of the flow system. This objective was achieved by developing three-dimensional viscous and inviscid computer codes to predict the pressure and temperature distributions in the engine flow passages, particularly within the SSME turbines and turnaround ducts.</description><identifier>ISSN: 0148-7191</identifier><identifier>EISSN: 2688-3627</identifier><identifier>DOI: 10.4271/841522</identifier><language>eng</language><creationdate>1984</creationdate><rights>Copyright 1984 Society of Automotive Engineers, Inc.</rights><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://doi.org/10.4271/841522$$EHTML$$P50$$Gsae$$H</linktohtml><link.rule.ids>776,780,26316,27901,79451,79455</link.rule.ids><linktorsrc>$$Uhttps://doi.org/10.4271/841522$$EView_record_in_SAE_Mobilus$$FView_record_in_$$GSAE_Mobilus</linktorsrc></links><search><creatorcontrib>Povinelli, Louis A</creatorcontrib><creatorcontrib>Haas, Jeffrey E</creatorcontrib><creatorcontrib>MeLallin, Kerry L</creatorcontrib><creatorcontrib>Schwab, John R</creatorcontrib><creatorcontrib>Chima, Rodrick V</creatorcontrib><title>Application of Viscous and Inviscid Computation Methods for Rocket Turbopump Systems</title><description>This paper examines current research efforts underway at Lewis Research Center which have focused on improving the structural durability of the SSME turbodrive system through more fully examining the aerothermodynamics of the flow system. This objective was achieved by developing three-dimensional viscous and inviscid computer codes to predict the pressure and temperature distributions in the engine flow passages, particularly within the SSME turbines and turnaround ducts.</description><issn>0148-7191</issn><issn>2688-3627</issn><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1984</creationdate><recordtype>report</recordtype><sourceid>AEUUQ</sourceid><recordid>eNqNjssKgkAYRocoyG7P8PcAljNeW4YUtWhT0lamcURLncF_DHr7BHuAVocPDnyHkBV1Nh4L6TbyqM_YiFgsiCLbDVg4JpZDvcgO6Y5OyQzx6Tgu9UPPIsle66oU3JSqAZXDvUShOgTeZHBu3v0qM4hVrTszOBdpCpUh5KqFqxIvaSDp2ofSXa3h9kEja1yQSc4rlMsf52R9PCTxyUYuUyNF0fSPleZatpgOue4_zhcnYkRX</recordid><startdate>19841001</startdate><enddate>19841001</enddate><creator>Povinelli, Louis A</creator><creator>Haas, Jeffrey E</creator><creator>MeLallin, Kerry L</creator><creator>Schwab, John R</creator><creator>Chima, Rodrick V</creator><scope>AEUUQ</scope></search><sort><creationdate>19841001</creationdate><title>Application of Viscous and Inviscid Computation Methods for Rocket Turbopump Systems</title><author>Povinelli, Louis A ; Haas, Jeffrey E ; MeLallin, Kerry L ; Schwab, John R ; Chima, Rodrick V</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-sae_technicalpapers_8415223</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1984</creationdate><toplevel>online_resources</toplevel><creatorcontrib>Povinelli, Louis A</creatorcontrib><creatorcontrib>Haas, Jeffrey E</creatorcontrib><creatorcontrib>MeLallin, Kerry L</creatorcontrib><creatorcontrib>Schwab, John R</creatorcontrib><creatorcontrib>Chima, Rodrick V</creatorcontrib><collection>SAE Technical Papers, Back File B (1980-1989)</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Povinelli, Louis A</au><au>Haas, Jeffrey E</au><au>MeLallin, Kerry L</au><au>Schwab, John R</au><au>Chima, Rodrick V</au><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Application of Viscous and Inviscid Computation Methods for Rocket Turbopump Systems</btitle><date>1984-10-01</date><risdate>1984</risdate><issn>0148-7191</issn><eissn>2688-3627</eissn><abstract>This paper examines current research efforts underway at Lewis Research Center which have focused on improving the structural durability of the SSME turbodrive system through more fully examining the aerothermodynamics of the flow system. This objective was achieved by developing three-dimensional viscous and inviscid computer codes to predict the pressure and temperature distributions in the engine flow passages, particularly within the SSME turbines and turnaround ducts.</abstract><doi>10.4271/841522</doi></addata></record>
fulltext fulltext_linktorsrc
identifier ISSN: 0148-7191
ispartof
issn 0148-7191
2688-3627
language eng
recordid cdi_sae_technicalpapers_841522
source SAE Technical Papers, Back File B (1980-1989)
title Application of Viscous and Inviscid Computation Methods for Rocket Turbopump Systems
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-24T07%3A41%3A45IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-sae_AEUUQ&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.btitle=Application%20of%20Viscous%20and%20Inviscid%20Computation%20Methods%20for%20Rocket%20Turbopump%20Systems&rft.au=Povinelli,%20Louis%20A&rft.date=1984-10-01&rft.issn=0148-7191&rft.eissn=2688-3627&rft_id=info:doi/10.4271/841522&rft_dat=%3Csae_AEUUQ%3E841522%3C/sae_AEUUQ%3E%3Cgrp_id%3Ecdi_FETCH-sae_technicalpapers_8415223%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true