DETERMINATION OF WINDS FROM METEOROLOGICAL ROCKETSONDES

The equations of motion are derived for an object falling under the influence of gravity and aerodynamic drag. These equations are used to examine the response of the ARCAS parachute to hypothetical wind profiles in the region extending from 30 to 80 km. A computational scheme for determining the ho...

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Hauptverfasser:	Eddy, Amos, duchon, C E, Haase, F M, Haragan, D R
Format:	Report
Sprache:	eng
Schlagworte:	ARCAS ATMOSPHERIC SOUNDING EQUATIONS OF MOTION Meteorology RADIOSONDES SOUNDING ROCKETS Unmanned Spacecraft WIND WIND DIRECTION INDICATORS
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creator	Eddy, Amos duchon, C E Haase, F M Haragan, D R
description	The equations of motion are derived for an object falling under the influence of gravity and aerodynamic drag. These equations are used to examine the response of the ARCAS parachute to hypothetical wind profiles in the region extending from 30 to 80 km. A computational scheme for determining the horizontal wind from the observed motion of any wind sensor influenced only by the above forces is presented, along with an example of its application to an ARCAS parachute flight.
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These equations are used to examine the response of the ARCAS parachute to hypothetical wind profiles in the region extending from 30 to 80 km. A computational scheme for determining the horizontal wind from the observed motion of any wind sensor influenced only by the above forces is presented, along with an example of its application to an ARCAS parachute flight.</description><language>eng</language><subject>ARCAS ; ATMOSPHERIC SOUNDING ; EQUATIONS OF MOTION ; Meteorology ; RADIOSONDES ; SOUNDING ROCKETS ; Unmanned Spacecraft ; WIND ; WIND DIRECTION INDICATORS</subject><creationdate>1965</creationdate><rights>Approved for public release; distribution is unlimited.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27546,27547</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0635185$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Eddy, Amos</creatorcontrib><creatorcontrib>duchon, C E</creatorcontrib><creatorcontrib>Haase, F M</creatorcontrib><creatorcontrib>Haragan, D R</creatorcontrib><creatorcontrib>TEXAS UNIV AT AUSTIN ATMOSPHERIC SCIENCE GROUP</creatorcontrib><title>DETERMINATION OF WINDS FROM METEOROLOGICAL ROCKETSONDES</title><description>The equations of motion are derived for an object falling under the influence of gravity and aerodynamic drag. These equations are used to examine the response of the ARCAS parachute to hypothetical wind profiles in the region extending from 30 to 80 km. A computational scheme for determining the horizontal wind from the observed motion of any wind sensor influenced only by the above forces is presented, along with an example of its application to an ARCAS parachute flight.</description><subject>ARCAS</subject><subject>ATMOSPHERIC SOUNDING</subject><subject>EQUATIONS OF MOTION</subject><subject>Meteorology</subject><subject>RADIOSONDES</subject><subject>SOUNDING ROCKETS</subject><subject>Unmanned Spacecraft</subject><subject>WIND</subject><subject>WIND DIRECTION INDICATORS</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1965</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZDB3cQ1xDfL19HMM8fT3U_B3Uwj39HMJVnAL8vdV8AXK-Qf5-_i7ezo7-igE-Tt7u4YE-_u5uAbzMLCmJeYUp_JCaW4GGTfXEGcP3ZSSzOT44pLMvNSSeEcXAzNjU0MLU2MC0gDPnCWb</recordid><startdate>196511</startdate><enddate>196511</enddate><creator>Eddy, Amos</creator><creator>duchon, C E</creator><creator>Haase, F M</creator><creator>Haragan, D R</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>196511</creationdate><title>DETERMINATION OF WINDS FROM METEOROLOGICAL ROCKETSONDES</title><author>Eddy, Amos ; duchon, C E ; Haase, F M ; Haragan, D R</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD06351853</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1965</creationdate><topic>ARCAS</topic><topic>ATMOSPHERIC SOUNDING</topic><topic>EQUATIONS OF MOTION</topic><topic>Meteorology</topic><topic>RADIOSONDES</topic><topic>SOUNDING ROCKETS</topic><topic>Unmanned Spacecraft</topic><topic>WIND</topic><topic>WIND DIRECTION INDICATORS</topic><toplevel>online_resources</toplevel><creatorcontrib>Eddy, Amos</creatorcontrib><creatorcontrib>duchon, C E</creatorcontrib><creatorcontrib>Haase, F M</creatorcontrib><creatorcontrib>Haragan, D R</creatorcontrib><creatorcontrib>TEXAS UNIV AT AUSTIN ATMOSPHERIC SCIENCE GROUP</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Eddy, Amos</au><au>duchon, C E</au><au>Haase, F M</au><au>Haragan, D R</au><aucorp>TEXAS UNIV AT AUSTIN ATMOSPHERIC SCIENCE GROUP</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>DETERMINATION OF WINDS FROM METEOROLOGICAL ROCKETSONDES</btitle><date>1965-11</date><risdate>1965</risdate><abstract>The equations of motion are derived for an object falling under the influence of gravity and aerodynamic drag. These equations are used to examine the response of the ARCAS parachute to hypothetical wind profiles in the region extending from 30 to 80 km. A computational scheme for determining the horizontal wind from the observed motion of any wind sensor influenced only by the above forces is presented, along with an example of its application to an ARCAS parachute flight.</abstract><oa>free_for_read</oa></addata></record>
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subjects	ARCAS ATMOSPHERIC SOUNDING EQUATIONS OF MOTION Meteorology RADIOSONDES SOUNDING ROCKETS Unmanned Spacecraft WIND WIND DIRECTION INDICATORS
title	DETERMINATION OF WINDS FROM METEOROLOGICAL ROCKETSONDES
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