Static Aeroelastic Considerations in the Definition of Design Loads for Fighter Airplanes
This paper first discusses some typical effects of static aeroelastic correction factors in context with the definition of structural design loads for major aircraft components. The influences on response parameters and resulting design loads are shown as well as the aeroelastic optimization of trai...
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| creator | Schmidinger, G Sensburg, O |
| description | This paper first discusses some typical effects of static aeroelastic correction factors in context with the definition of structural design loads for major aircraft components. The influences on response parameters and resulting design loads are shown as well as the aeroelastic optimization of trailing edge flaps with respect to geometry, efficiency and hinge moments.
This article is from 'Static Aeroelastic Effects on High Performance Aircraft', AD-A199 170, p3-1 thru 3-20. |
| format | Report |
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This article is from 'Static Aeroelastic Effects on High Performance Aircraft', AD-A199 170, p3-1 thru 3-20.</description><language>eng</language><subject>AERODYNAMIC CONTROL SURFACES ; AERODYNAMIC LOADING ; Aerodynamics ; AEROELASTICITY ; AIRCRAFT ; Component reports ; CORRECTIONS ; FLAPS(CONTROL SURFACES) ; Fluid Mechanics ; MATHEMATICAL MODELS ; OPTIMIZATION ; STATICS ; STRUCTURAL COMPONENTS ; Structural loads ; WEST GERMANY</subject><creationdate>1986</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/ADP005856$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Schmidinger, G</creatorcontrib><creatorcontrib>Sensburg, O</creatorcontrib><creatorcontrib>MESSERSCHMITT-BOELKOW-BLOHM G M B H MUNICH (GERMANY F R)</creatorcontrib><title>Static Aeroelastic Considerations in the Definition of Design Loads for Fighter Airplanes</title><description>This paper first discusses some typical effects of static aeroelastic correction factors in context with the definition of structural design loads for major aircraft components. The influences on response parameters and resulting design loads are shown as well as the aeroelastic optimization of trailing edge flaps with respect to geometry, efficiency and hinge moments.
This article is from 'Static Aeroelastic Effects on High Performance Aircraft', AD-A199 170, p3-1 thru 3-20.</description><subject>AERODYNAMIC CONTROL SURFACES</subject><subject>AERODYNAMIC LOADING</subject><subject>Aerodynamics</subject><subject>AEROELASTICITY</subject><subject>AIRCRAFT</subject><subject>Component reports</subject><subject>CORRECTIONS</subject><subject>FLAPS(CONTROL SURFACES)</subject><subject>Fluid Mechanics</subject><subject>MATHEMATICAL MODELS</subject><subject>OPTIMIZATION</subject><subject>STATICS</subject><subject>STRUCTURAL COMPONENTS</subject><subject>Structural loads</subject><subject>WEST GERMANY</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1986</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZIgMLkksyUxWcEwtyk_NSSwGsZ3z84ozU1KLgBJAlkJmnkJJRqqCS2paZl4mSEghPw3IK85Mz1PwyU9MKVZIyy9ScMtMzyhJLVJwzCwqyEnMSy3mYWBNS8wpTuWF0twMMm6uIc4euilAO-KBFuWllsQ7ugQYGJhamJoZE5AGAG1MN3U</recordid><startdate>19861003</startdate><enddate>19861003</enddate><creator>Schmidinger, G</creator><creator>Sensburg, O</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>19861003</creationdate><title>Static Aeroelastic Considerations in the Definition of Design Loads for Fighter Airplanes</title><author>Schmidinger, G ; Sensburg, O</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADP0058563</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1986</creationdate><topic>AERODYNAMIC CONTROL SURFACES</topic><topic>AERODYNAMIC LOADING</topic><topic>Aerodynamics</topic><topic>AEROELASTICITY</topic><topic>AIRCRAFT</topic><topic>Component reports</topic><topic>CORRECTIONS</topic><topic>FLAPS(CONTROL SURFACES)</topic><topic>Fluid Mechanics</topic><topic>MATHEMATICAL MODELS</topic><topic>OPTIMIZATION</topic><topic>STATICS</topic><topic>STRUCTURAL COMPONENTS</topic><topic>Structural loads</topic><topic>WEST GERMANY</topic><toplevel>online_resources</toplevel><creatorcontrib>Schmidinger, G</creatorcontrib><creatorcontrib>Sensburg, O</creatorcontrib><creatorcontrib>MESSERSCHMITT-BOELKOW-BLOHM G M B H MUNICH (GERMANY F R)</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Schmidinger, G</au><au>Sensburg, O</au><aucorp>MESSERSCHMITT-BOELKOW-BLOHM G M B H MUNICH (GERMANY F R)</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Static Aeroelastic Considerations in the Definition of Design Loads for Fighter Airplanes</btitle><date>1986-10-03</date><risdate>1986</risdate><abstract>This paper first discusses some typical effects of static aeroelastic correction factors in context with the definition of structural design loads for major aircraft components. The influences on response parameters and resulting design loads are shown as well as the aeroelastic optimization of trailing edge flaps with respect to geometry, efficiency and hinge moments.
This article is from 'Static Aeroelastic Effects on High Performance Aircraft', AD-A199 170, p3-1 thru 3-20.</abstract><oa>free_for_read</oa></addata></record> |
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| source | DTIC Technical Reports |
| subjects | AERODYNAMIC CONTROL SURFACES AERODYNAMIC LOADING Aerodynamics AEROELASTICITY AIRCRAFT Component reports CORRECTIONS FLAPS(CONTROL SURFACES) Fluid Mechanics MATHEMATICAL MODELS OPTIMIZATION STATICS STRUCTURAL COMPONENTS Structural loads WEST GERMANY |
| title | Static Aeroelastic Considerations in the Definition of Design Loads for Fighter Airplanes |
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