Response of Aircraft to Three Dimensional Random Turbulence
PROCEDURES FOR DESIGNING AIRCRAFT FOR THE COMBINED EFFECTS OF VERTICAL, LATERAL, AND LONGITUDINAL TURBULENCE BY THE APPLICATION OF POWER SPECTRAL TECHNIQUES ARE DEVELOPED AND OUTLINED. The present state-of-the-art of this technical area is established and evaluated by reviewing and extending current...
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| creator | Eichenbaum,Frederick D |
| description | PROCEDURES FOR DESIGNING AIRCRAFT FOR THE COMBINED EFFECTS OF VERTICAL, LATERAL, AND LONGITUDINAL TURBULENCE BY THE APPLICATION OF POWER SPECTRAL TECHNIQUES ARE DEVELOPED AND OUTLINED. The present state-of-the-art of this technical area is established and evaluated by reviewing and extending current methods used or proposed for predicting the response of aircraft due to combined effects of the three components of atmospheric turbulence. Requirements for solving the problem are identified and recommendations are made with respect to major problem areas such as: description of the turbulence environment, determination of the frequency response function of the structure, and methods of combining the effects of vertical, lateral and longitudinal turbulence components to theoretically predict aircraft response. (Author Modified Abstract) |
| format | Report |
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The present state-of-the-art of this technical area is established and evaluated by reviewing and extending current methods used or proposed for predicting the response of aircraft due to combined effects of the three components of atmospheric turbulence. Requirements for solving the problem are identified and recommendations are made with respect to major problem areas such as: description of the turbulence environment, determination of the frequency response function of the structure, and methods of combining the effects of vertical, lateral and longitudinal turbulence components to theoretically predict aircraft response. (Author Modified Abstract)</description><language>eng</language><subject>AERODYNAMIC CONTROL SURFACES ; AEROSTATICS ; Aircraft ; AIRFRAMES ; BUFFETING ; DYNAMIC RESPONSE ; GUST LOADS ; MATHEMATICAL MODELS ; Mechanics ; POWER SPECTRA ; TRANSFER FUNCTIONS ; TURBULENCE</subject><creationdate>1972</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27544,27545</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0756886$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Eichenbaum,Frederick D</creatorcontrib><creatorcontrib>LOCKHEED-GEORGIA CO MARIETTA</creatorcontrib><title>Response of Aircraft to Three Dimensional Random Turbulence</title><description>PROCEDURES FOR DESIGNING AIRCRAFT FOR THE COMBINED EFFECTS OF VERTICAL, LATERAL, AND LONGITUDINAL TURBULENCE BY THE APPLICATION OF POWER SPECTRAL TECHNIQUES ARE DEVELOPED AND OUTLINED. The present state-of-the-art of this technical area is established and evaluated by reviewing and extending current methods used or proposed for predicting the response of aircraft due to combined effects of the three components of atmospheric turbulence. Requirements for solving the problem are identified and recommendations are made with respect to major problem areas such as: description of the turbulence environment, determination of the frequency response function of the structure, and methods of combining the effects of vertical, lateral and longitudinal turbulence components to theoretically predict aircraft response. (Author Modified Abstract)</description><subject>AERODYNAMIC CONTROL SURFACES</subject><subject>AEROSTATICS</subject><subject>Aircraft</subject><subject>AIRFRAMES</subject><subject>BUFFETING</subject><subject>DYNAMIC RESPONSE</subject><subject>GUST LOADS</subject><subject>MATHEMATICAL MODELS</subject><subject>Mechanics</subject><subject>POWER SPECTRA</subject><subject>TRANSFER FUNCTIONS</subject><subject>TURBULENCE</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1972</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZLAOSi0uyM8rTlXIT1NwzCxKLkpMK1EoyVcIyShKTVVwycxNzSvOzM9LzFEISsxLyc9VCCktSirNSc1LTuVhYE1LzClO5YXS3Awybq4hzh66KSWZyfHFJZl5qSXxji4G5qZmFhZmxgSkAbKgLEQ</recordid><startdate>197210</startdate><enddate>197210</enddate><creator>Eichenbaum,Frederick D</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>197210</creationdate><title>Response of Aircraft to Three Dimensional Random Turbulence</title><author>Eichenbaum,Frederick D</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD07568863</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1972</creationdate><topic>AERODYNAMIC CONTROL SURFACES</topic><topic>AEROSTATICS</topic><topic>Aircraft</topic><topic>AIRFRAMES</topic><topic>BUFFETING</topic><topic>DYNAMIC RESPONSE</topic><topic>GUST LOADS</topic><topic>MATHEMATICAL MODELS</topic><topic>Mechanics</topic><topic>POWER SPECTRA</topic><topic>TRANSFER FUNCTIONS</topic><topic>TURBULENCE</topic><toplevel>online_resources</toplevel><creatorcontrib>Eichenbaum,Frederick D</creatorcontrib><creatorcontrib>LOCKHEED-GEORGIA CO MARIETTA</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Eichenbaum,Frederick D</au><aucorp>LOCKHEED-GEORGIA CO MARIETTA</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Response of Aircraft to Three Dimensional Random Turbulence</btitle><date>1972-10</date><risdate>1972</risdate><abstract>PROCEDURES FOR DESIGNING AIRCRAFT FOR THE COMBINED EFFECTS OF VERTICAL, LATERAL, AND LONGITUDINAL TURBULENCE BY THE APPLICATION OF POWER SPECTRAL TECHNIQUES ARE DEVELOPED AND OUTLINED. The present state-of-the-art of this technical area is established and evaluated by reviewing and extending current methods used or proposed for predicting the response of aircraft due to combined effects of the three components of atmospheric turbulence. Requirements for solving the problem are identified and recommendations are made with respect to major problem areas such as: description of the turbulence environment, determination of the frequency response function of the structure, and methods of combining the effects of vertical, lateral and longitudinal turbulence components to theoretically predict aircraft response. (Author Modified Abstract)</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| source | DTIC Technical Reports |
| subjects | AERODYNAMIC CONTROL SURFACES AEROSTATICS Aircraft AIRFRAMES BUFFETING DYNAMIC RESPONSE GUST LOADS MATHEMATICAL MODELS Mechanics POWER SPECTRA TRANSFER FUNCTIONS TURBULENCE |
| title | Response of Aircraft to Three Dimensional Random Turbulence |
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