Subsonic static and dynamic stability characteristics of a NASP configuration
Wind-tunnel tests of a National Aero-Space Plane configuration were conducted, and the model used was a LaRC designed blended body configuration. The Aerodynmaic Preliminary Analysis System damping predictions were good for the roll mode and only fair for the pitch and yaw modes.
Gespeichert in:
| Veröffentlicht in: | Journal of aircraft 1994-07, Vol.31 (4), p.879-885 |
|---|---|
| Hauptverfasser: | , , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 885 |
|---|---|
| container_issue | 4 |
| container_start_page | 879 |
| container_title | Journal of aircraft |
| container_volume | 31 |
| creator | BOYDEN, R. P DRESS, D. A FOX, C. H HUFFMAN, J. K CRUZ, C. I |
| description | Wind-tunnel tests of a National Aero-Space Plane configuration were conducted, and the model used was a LaRC designed blended body configuration. The Aerodynmaic Preliminary Analysis System damping predictions were good for the roll mode and only fair for the pitch and yaw modes. |
| doi_str_mv | 10.2514/3.46574 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_pasca</sourceid><recordid>TN_cdi_proquest_journals_207624376</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2723222</sourcerecordid><originalsourceid>FETCH-LOGICAL-p141t-9033aa5642d971fa2a6d580f4e831d03846257bfa50070a2a6cfb20a3302c3533</originalsourceid><addsrcrecordid>eNotj0tLAzEUhYMoWKv4F4K4nXrzTpel-IL6gOp6uJOZaEqbqcnMov_eSF0dOPc793AIuWYw44rJOzGTWhl5QiZMCVEJq-0pmQBwVlmt5-fkIucNAFgwZkJe1mOT-xgczQMORTC2tD1E3B2tJmzDcKDuGxO6oUshFyjT3lOkr4v1O3V99OFrTCXcx0ty5nGbu6t_nZLPh_uP5VO1ent8Xi5W1Z5JNlRzEAJRacnbuWEeOepWWfCys4K1IKzUXJnGowIw8Hd2vuGAQgB3oqyakpvj333qf8YuD_WmH1MslTUHo7kURhfo9h_C7HDrE0YXcr1PYYfpUEteWrQSv78LWZ0</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>207624376</pqid></control><display><type>article</type><title>Subsonic static and dynamic stability characteristics of a NASP configuration</title><source>Alma/SFX Local Collection</source><creator>BOYDEN, R. P ; DRESS, D. A ; FOX, C. H ; HUFFMAN, J. K ; CRUZ, C. I</creator><creatorcontrib>BOYDEN, R. P ; DRESS, D. A ; FOX, C. H ; HUFFMAN, J. K ; CRUZ, C. I</creatorcontrib><description>Wind-tunnel tests of a National Aero-Space Plane configuration were conducted, and the model used was a LaRC designed blended body configuration. The Aerodynmaic Preliminary Analysis System damping predictions were good for the roll mode and only fair for the pitch and yaw modes.</description><identifier>ISSN: 0021-8669</identifier><identifier>EISSN: 1533-3868</identifier><identifier>DOI: 10.2514/3.46574</identifier><identifier>CODEN: JAIRAM</identifier><language>eng</language><publisher>Reston, VA: American Institute of Aeronautics and Astronautics</publisher><subject>Aerodynamics ; Aircraft ; Applied fluid mechanics ; Exact sciences and technology ; Fluid dynamics ; Fundamental areas of phenomenology (including applications) ; Physics ; Tests ; Wind tunnels</subject><ispartof>Journal of aircraft, 1994-07, Vol.31 (4), p.879-885</ispartof><rights>1994 INIST-CNRS</rights><rights>Copyright American Institute of Aeronautics and Astronautics Jul 1994</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>309,310,314,776,780,785,786,23909,23910,25118,27901,27902</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=4246265$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>BOYDEN, R. P</creatorcontrib><creatorcontrib>DRESS, D. A</creatorcontrib><creatorcontrib>FOX, C. H</creatorcontrib><creatorcontrib>HUFFMAN, J. K</creatorcontrib><creatorcontrib>CRUZ, C. I</creatorcontrib><title>Subsonic static and dynamic stability characteristics of a NASP configuration</title><title>Journal of aircraft</title><description>Wind-tunnel tests of a National Aero-Space Plane configuration were conducted, and the model used was a LaRC designed blended body configuration. The Aerodynmaic Preliminary Analysis System damping predictions were good for the roll mode and only fair for the pitch and yaw modes.</description><subject>Aerodynamics</subject><subject>Aircraft</subject><subject>Applied fluid mechanics</subject><subject>Exact sciences and technology</subject><subject>Fluid dynamics</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Physics</subject><subject>Tests</subject><subject>Wind tunnels</subject><issn>0021-8669</issn><issn>1533-3868</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1994</creationdate><recordtype>article</recordtype><recordid>eNotj0tLAzEUhYMoWKv4F4K4nXrzTpel-IL6gOp6uJOZaEqbqcnMov_eSF0dOPc793AIuWYw44rJOzGTWhl5QiZMCVEJq-0pmQBwVlmt5-fkIucNAFgwZkJe1mOT-xgczQMORTC2tD1E3B2tJmzDcKDuGxO6oUshFyjT3lOkr4v1O3V99OFrTCXcx0ty5nGbu6t_nZLPh_uP5VO1ent8Xi5W1Z5JNlRzEAJRacnbuWEeOepWWfCys4K1IKzUXJnGowIw8Hd2vuGAQgB3oqyakpvj333qf8YuD_WmH1MslTUHo7kURhfo9h_C7HDrE0YXcr1PYYfpUEteWrQSv78LWZ0</recordid><startdate>19940701</startdate><enddate>19940701</enddate><creator>BOYDEN, R. P</creator><creator>DRESS, D. A</creator><creator>FOX, C. H</creator><creator>HUFFMAN, J. K</creator><creator>CRUZ, C. I</creator><general>American Institute of Aeronautics and Astronautics</general><scope>IQODW</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><scope>U9A</scope></search><sort><creationdate>19940701</creationdate><title>Subsonic static and dynamic stability characteristics of a NASP configuration</title><author>BOYDEN, R. P ; DRESS, D. A ; FOX, C. H ; HUFFMAN, J. K ; CRUZ, C. I</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p141t-9033aa5642d971fa2a6d580f4e831d03846257bfa50070a2a6cfb20a3302c3533</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1994</creationdate><topic>Aerodynamics</topic><topic>Aircraft</topic><topic>Applied fluid mechanics</topic><topic>Exact sciences and technology</topic><topic>Fluid dynamics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Physics</topic><topic>Tests</topic><topic>Wind tunnels</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>BOYDEN, R. P</creatorcontrib><creatorcontrib>DRESS, D. A</creatorcontrib><creatorcontrib>FOX, C. H</creatorcontrib><creatorcontrib>HUFFMAN, J. K</creatorcontrib><creatorcontrib>CRUZ, C. I</creatorcontrib><collection>Pascal-Francis</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of aircraft</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>BOYDEN, R. P</au><au>DRESS, D. A</au><au>FOX, C. H</au><au>HUFFMAN, J. K</au><au>CRUZ, C. I</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Subsonic static and dynamic stability characteristics of a NASP configuration</atitle><jtitle>Journal of aircraft</jtitle><date>1994-07-01</date><risdate>1994</risdate><volume>31</volume><issue>4</issue><spage>879</spage><epage>885</epage><pages>879-885</pages><issn>0021-8669</issn><eissn>1533-3868</eissn><coden>JAIRAM</coden><abstract>Wind-tunnel tests of a National Aero-Space Plane configuration were conducted, and the model used was a LaRC designed blended body configuration. The Aerodynmaic Preliminary Analysis System damping predictions were good for the roll mode and only fair for the pitch and yaw modes.</abstract><cop>Reston, VA</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/3.46574</doi><tpages>7</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0021-8669 |
| ispartof | Journal of aircraft, 1994-07, Vol.31 (4), p.879-885 |
| issn | 0021-8669 1533-3868 |
| language | eng |
| recordid | cdi_proquest_journals_207624376 |
| source | Alma/SFX Local Collection |
| subjects | Aerodynamics Aircraft Applied fluid mechanics Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Physics Tests Wind tunnels |
| title | Subsonic static and dynamic stability characteristics of a NASP configuration |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-13T23%3A27%3A57IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_pasca&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Subsonic%20static%20and%20dynamic%20stability%20characteristics%20of%20a%20NASP%20configuration&rft.jtitle=Journal%20of%20aircraft&rft.au=BOYDEN,%20R.%20P&rft.date=1994-07-01&rft.volume=31&rft.issue=4&rft.spage=879&rft.epage=885&rft.pages=879-885&rft.issn=0021-8669&rft.eissn=1533-3868&rft.coden=JAIRAM&rft_id=info:doi/10.2514/3.46574&rft_dat=%3Cproquest_pasca%3E2723222%3C/proquest_pasca%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=207624376&rft_id=info:pmid/&rfr_iscdi=true |