Transonic static and dynamic stability characteristics of a finned projectile configuration

Transonic static and dynamic stability characteristics of a finned projectile configuration

Static and dynamic stability tests were made of a finned projectile configuration with the aft-mounted fins arranged in a cruciform pattern. The tests were made at free stream Mach numbers of 0.7, 0.9, 1.1, and 1.2 in the Langley 8-foot transonic pressure tunnel. Some of the parameters measured duri...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Boyden, R. P., Brooks, C. W., Jr, Davenport, E. E.
Format: Report
Sprache:eng
Schlagworte:
Aerodynamics
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator Boyden, R. P.
Brooks, C. W., Jr
Davenport, E. E.
description Static and dynamic stability tests were made of a finned projectile configuration with the aft-mounted fins arranged in a cruciform pattern. The tests were made at free stream Mach numbers of 0.7, 0.9, 1.1, and 1.2 in the Langley 8-foot transonic pressure tunnel. Some of the parameters measured during the tests were lift, drag, pitching moment, pitch damping, and roll damping. Configurations tested included the body with undeflected fins, the body with various fin deflections for control, and the body with fins removed. Theoretical estimates of the stability derivatives were made for the fins on configuration.
format Report
fullrecord <record><control><sourceid>nasa_CYI</sourceid><recordid>TN_cdi_nasa_ntrs_19780012129</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>19780012129</sourcerecordid><originalsourceid>FETCH-nasa_ntrs_197800121293</originalsourceid><addsrcrecordid>eNqFjDsOwkAMBdNQIOAGFL4AUjYUkBqBOEA6isjsB4wWL7JNkduzEvRUI715mnlzGQRZC5MHNbQK5ABhYnx-pytlsgn8HQW9RSGtJ4WSACERcwzwkvKI3ihH8IUT3d5SS4WXzSxh1rj6cdGsT8fhcN4wKo5soqPrd_u2dZ3r-u0f_QFYDDg1</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Transonic static and dynamic stability characteristics of a finned projectile configuration</title><source>NASA Technical Reports Server</source><creator>Boyden, R. P. ; Brooks, C. W., Jr ; Davenport, E. E.</creator><creatorcontrib>Boyden, R. P. ; Brooks, C. W., Jr ; Davenport, E. E.</creatorcontrib><description>Static and dynamic stability tests were made of a finned projectile configuration with the aft-mounted fins arranged in a cruciform pattern. The tests were made at free stream Mach numbers of 0.7, 0.9, 1.1, and 1.2 in the Langley 8-foot transonic pressure tunnel. Some of the parameters measured during the tests were lift, drag, pitching moment, pitch damping, and roll damping. Configurations tested included the body with undeflected fins, the body with various fin deflections for control, and the body with fins removed. Theoretical estimates of the stability derivatives were made for the fins on configuration.</description><language>eng</language><publisher>Legacy CDMS</publisher><subject>Aerodynamics</subject><creationdate>1978</creationdate><rights>Copyright Determination: GOV_PUBLIC_USE_PERMITTED</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>780,800</link.rule.ids><linktorsrc>$$Uhttps://ntrs.nasa.gov/citations/19780012129$$EView_record_in_NASA$$FView_record_in_$$GNASA$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Boyden, R. P.</creatorcontrib><creatorcontrib>Brooks, C. W., Jr</creatorcontrib><creatorcontrib>Davenport, E. E.</creatorcontrib><title>Transonic static and dynamic stability characteristics of a finned projectile configuration</title><description>Static and dynamic stability tests were made of a finned projectile configuration with the aft-mounted fins arranged in a cruciform pattern. The tests were made at free stream Mach numbers of 0.7, 0.9, 1.1, and 1.2 in the Langley 8-foot transonic pressure tunnel. Some of the parameters measured during the tests were lift, drag, pitching moment, pitch damping, and roll damping. Configurations tested included the body with undeflected fins, the body with various fin deflections for control, and the body with fins removed. Theoretical estimates of the stability derivatives were made for the fins on configuration.</description><subject>Aerodynamics</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1978</creationdate><recordtype>report</recordtype><sourceid>CYI</sourceid><recordid>eNqFjDsOwkAMBdNQIOAGFL4AUjYUkBqBOEA6isjsB4wWL7JNkduzEvRUI715mnlzGQRZC5MHNbQK5ABhYnx-pytlsgn8HQW9RSGtJ4WSACERcwzwkvKI3ihH8IUT3d5SS4WXzSxh1rj6cdGsT8fhcN4wKo5soqPrd_u2dZ3r-u0f_QFYDDg1</recordid><startdate>19780401</startdate><enddate>19780401</enddate><creator>Boyden, R. P.</creator><creator>Brooks, C. W., Jr</creator><creator>Davenport, E. E.</creator><scope>CYE</scope><scope>CYI</scope></search><sort><creationdate>19780401</creationdate><title>Transonic static and dynamic stability characteristics of a finned projectile configuration</title><author>Boyden, R. P. ; Brooks, C. W., Jr ; Davenport, E. E.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-nasa_ntrs_197800121293</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1978</creationdate><topic>Aerodynamics</topic><toplevel>online_resources</toplevel><creatorcontrib>Boyden, R. P.</creatorcontrib><creatorcontrib>Brooks, C. W., Jr</creatorcontrib><creatorcontrib>Davenport, E. E.</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Boyden, R. P.</au><au>Brooks, C. W., Jr</au><au>Davenport, E. E.</au><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Transonic static and dynamic stability characteristics of a finned projectile configuration</btitle><date>1978-04-01</date><risdate>1978</risdate><abstract>Static and dynamic stability tests were made of a finned projectile configuration with the aft-mounted fins arranged in a cruciform pattern. The tests were made at free stream Mach numbers of 0.7, 0.9, 1.1, and 1.2 in the Langley 8-foot transonic pressure tunnel. Some of the parameters measured during the tests were lift, drag, pitching moment, pitch damping, and roll damping. Configurations tested included the body with undeflected fins, the body with various fin deflections for control, and the body with fins removed. Theoretical estimates of the stability derivatives were made for the fins on configuration.</abstract><cop>Legacy CDMS</cop><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_nasa_ntrs_19780012129
source NASA Technical Reports Server
subjects Aerodynamics
title Transonic static and dynamic stability characteristics of a finned projectile configuration
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-15T04%3A56%3A05IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-nasa_CYI&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.btitle=Transonic%20static%20and%20dynamic%20stability%20characteristics%20of%20a%20finned%20projectile%20configuration&rft.au=Boyden,%20R.%20P.&rft.date=1978-04-01&rft_id=info:doi/&rft_dat=%3Cnasa_CYI%3E19780012129%3C/nasa_CYI%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true