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The Shock Vibration Bulletin. Part 4. Structural Dynamics and Modal Test and Analysis
Contents: Qualification by analysis of Inertial Upper Stage Plume deflectors; Analysis of reinforced concrete structures under the effects of localized detonations; Reinforced concrete arches under blast and shock environment; Dynamic stress at critical locations of a structure as a criterion for ma...
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| creator | NAVAL RESEARCH LAB WASHINGTON DC SHOCK AND VIBRATION INFORMATION CENTER |
| description | Contents: Qualification by analysis of Inertial Upper Stage Plume deflectors; Analysis of reinforced concrete structures under the effects of localized detonations; Reinforced concrete arches under blast and shock environment; Dynamic stress at critical locations of a structure as a criterion for mathematical model modification; Optimized structure design using reanalysis techniques; Reliability of structures with stiffness and strength degradation; New look at the use of linear methods to predict aircraft dynamic response to taxi over bomb-damaged and repaired airfields; Frequency response functions of a nonlinear system; System characterization in nonlinear random vibration; Interactive-graphics method for dynamic system modelling applying consistency rules; Dynamic response of a geared train of rotors subjected to random support excitations; Dynamics of an oscillating four-bar linkage: Modal test and analysis -- Centaur G modal test.
See also Part 1, AD-A186 748. |
| format | report |
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See also Part 1, AD-A186 748.</description><language>eng</language><subject>AIRCRAFT ; ARCHES ; BLAST ; BOMB DAMAGE ; CONSISTENCY ; DEGRADATION ; DETONATIONS ; DYNAMIC RESPONSE ; DYNAMICS ; FREQUENCY RESPONSE ; INTERACTIVE GRAPHICS ; LANDING FIELDS ; LINKAGES ; MATHEMATICAL MODELS ; MATHEMATICAL PREDICTION ; Mechanics ; MODIFICATION ; NONLINEAR SYSTEMS ; OPTIMIZATION ; PERIODICALS ; POSITION(LOCATION) ; RANDOM VIBRATION ; REINFORCED CONCRETE ; RELIABILITY ; ROTORS ; SHOCK ; SHOCK(MECHANICS) ; STIFFNESS ; STRENGTH(MECHANICS) ; STRESSES ; STRUCTURAL DYNAMICS ; STRUCTURAL PROPERTIES ; STRUCTURAL RESPONSE ; STRUCTURES ; SYMPOSIA ; TAXIING ; VIBRATION</subject><creationdate>1987</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>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27543,27544</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA186751$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NAVAL RESEARCH LAB WASHINGTON DC SHOCK AND VIBRATION INFORMATION CENTER</creatorcontrib><title>The Shock Vibration Bulletin. Part 4. Structural Dynamics and Modal Test and Analysis</title><description>Contents: Qualification by analysis of Inertial Upper Stage Plume deflectors; Analysis of reinforced concrete structures under the effects of localized detonations; Reinforced concrete arches under blast and shock environment; Dynamic stress at critical locations of a structure as a criterion for mathematical model modification; Optimized structure design using reanalysis techniques; Reliability of structures with stiffness and strength degradation; New look at the use of linear methods to predict aircraft dynamic response to taxi over bomb-damaged and repaired airfields; Frequency response functions of a nonlinear system; System characterization in nonlinear random vibration; Interactive-graphics method for dynamic system modelling applying consistency rules; Dynamic response of a geared train of rotors subjected to random support excitations; Dynamics of an oscillating four-bar linkage: Modal test and analysis -- Centaur G modal test.
See also Part 1, AD-A186 748.</description><subject>AIRCRAFT</subject><subject>ARCHES</subject><subject>BLAST</subject><subject>BOMB DAMAGE</subject><subject>CONSISTENCY</subject><subject>DEGRADATION</subject><subject>DETONATIONS</subject><subject>DYNAMIC RESPONSE</subject><subject>DYNAMICS</subject><subject>FREQUENCY RESPONSE</subject><subject>INTERACTIVE GRAPHICS</subject><subject>LANDING FIELDS</subject><subject>LINKAGES</subject><subject>MATHEMATICAL MODELS</subject><subject>MATHEMATICAL PREDICTION</subject><subject>Mechanics</subject><subject>MODIFICATION</subject><subject>NONLINEAR SYSTEMS</subject><subject>OPTIMIZATION</subject><subject>PERIODICALS</subject><subject>POSITION(LOCATION)</subject><subject>RANDOM VIBRATION</subject><subject>REINFORCED CONCRETE</subject><subject>RELIABILITY</subject><subject>ROTORS</subject><subject>SHOCK</subject><subject>SHOCK(MECHANICS)</subject><subject>STIFFNESS</subject><subject>STRENGTH(MECHANICS)</subject><subject>STRESSES</subject><subject>STRUCTURAL DYNAMICS</subject><subject>STRUCTURAL PROPERTIES</subject><subject>STRUCTURAL RESPONSE</subject><subject>STRUCTURES</subject><subject>SYMPOSIA</subject><subject>TAXIING</subject><subject>VIBRATION</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1987</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZAgNyUhVCM7IT85WCMtMKkosyczPU3AqzclJLcnM01MISCwqUTDRUwguKSpNLiktSsxRcKnMS8zNTC5WSMxLUfDNTwEKhaQWl4C5jnmJOZXFmcU8DKxpiTnFqbxQmptBxs01xNlDN6UkMzm-GGh0akm8o4ujoYWZuamhMQFpANrYNMU</recordid><startdate>198701</startdate><enddate>198701</enddate><creator>NAVAL RESEARCH LAB WASHINGTON DC SHOCK AND VIBRATION INFORMATION CENTER</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>198701</creationdate><title>The Shock Vibration Bulletin. Part 4. Structural Dynamics and Modal Test and Analysis</title></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA1867513</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1987</creationdate><topic>AIRCRAFT</topic><topic>ARCHES</topic><topic>BLAST</topic><topic>BOMB DAMAGE</topic><topic>CONSISTENCY</topic><topic>DEGRADATION</topic><topic>DETONATIONS</topic><topic>DYNAMIC RESPONSE</topic><topic>DYNAMICS</topic><topic>FREQUENCY RESPONSE</topic><topic>INTERACTIVE GRAPHICS</topic><topic>LANDING FIELDS</topic><topic>LINKAGES</topic><topic>MATHEMATICAL MODELS</topic><topic>MATHEMATICAL PREDICTION</topic><topic>Mechanics</topic><topic>MODIFICATION</topic><topic>NONLINEAR SYSTEMS</topic><topic>OPTIMIZATION</topic><topic>PERIODICALS</topic><topic>POSITION(LOCATION)</topic><topic>RANDOM VIBRATION</topic><topic>REINFORCED CONCRETE</topic><topic>RELIABILITY</topic><topic>ROTORS</topic><topic>SHOCK</topic><topic>SHOCK(MECHANICS)</topic><topic>STIFFNESS</topic><topic>STRENGTH(MECHANICS)</topic><topic>STRESSES</topic><topic>STRUCTURAL DYNAMICS</topic><topic>STRUCTURAL PROPERTIES</topic><topic>STRUCTURAL RESPONSE</topic><topic>STRUCTURES</topic><topic>SYMPOSIA</topic><topic>TAXIING</topic><topic>VIBRATION</topic><toplevel>online_resources</toplevel><creatorcontrib>NAVAL RESEARCH LAB WASHINGTON DC SHOCK AND VIBRATION INFORMATION CENTER</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><aucorp>NAVAL RESEARCH LAB WASHINGTON DC SHOCK AND VIBRATION INFORMATION CENTER</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>The Shock Vibration Bulletin. Part 4. Structural Dynamics and Modal Test and Analysis</btitle><date>1987-01</date><risdate>1987</risdate><abstract>Contents: Qualification by analysis of Inertial Upper Stage Plume deflectors; Analysis of reinforced concrete structures under the effects of localized detonations; Reinforced concrete arches under blast and shock environment; Dynamic stress at critical locations of a structure as a criterion for mathematical model modification; Optimized structure design using reanalysis techniques; Reliability of structures with stiffness and strength degradation; New look at the use of linear methods to predict aircraft dynamic response to taxi over bomb-damaged and repaired airfields; Frequency response functions of a nonlinear system; System characterization in nonlinear random vibration; Interactive-graphics method for dynamic system modelling applying consistency rules; Dynamic response of a geared train of rotors subjected to random support excitations; Dynamics of an oscillating four-bar linkage: Modal test and analysis -- Centaur G modal test.
See also Part 1, AD-A186 748.</abstract><oa>free_for_read</oa></addata></record> |
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| source | DTIC Technical Reports |
| subjects | AIRCRAFT ARCHES BLAST BOMB DAMAGE CONSISTENCY DEGRADATION DETONATIONS DYNAMIC RESPONSE DYNAMICS FREQUENCY RESPONSE INTERACTIVE GRAPHICS LANDING FIELDS LINKAGES MATHEMATICAL MODELS MATHEMATICAL PREDICTION Mechanics MODIFICATION NONLINEAR SYSTEMS OPTIMIZATION PERIODICALS POSITION(LOCATION) RANDOM VIBRATION REINFORCED CONCRETE RELIABILITY ROTORS SHOCK SHOCK(MECHANICS) STIFFNESS STRENGTH(MECHANICS) STRESSES STRUCTURAL DYNAMICS STRUCTURAL PROPERTIES STRUCTURAL RESPONSE STRUCTURES SYMPOSIA TAXIING VIBRATION |
| title | The Shock Vibration Bulletin. Part 4. Structural Dynamics and Modal Test and Analysis |
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