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    Runout Path of an Airplane Equipped With Skids

    Source: Journal of Manufacturing Science and Engineering:;1962:;volume( 084 ):;issue: 003::page 301
    Author:
    Ching-U Ip
    DOI: 10.1115/1.3667481
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Equations of motion of the airplane subject to the influence of cross wind, rudder steering, and drag chute, during runout, are developed which would be valid even when the direction-of-travel angle and the yaw angle are large. A procedure of synthesizing the runout path step by step explicitly is presented. A flight vehicle capable of orbiting around the earth usually does not have ground steering capability because its weight has to be held to a minimum. This study will enable a designer to determine whether or not the vehicle will have inherent stability to land on a runway.
    keyword(s): Aircraft , Vehicles , Travel , Wind , Yaw , Flight , Weight (Mass) , Stability , Drag (Fluid dynamics) AND Equations of motion ,
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      Runout Path of an Airplane Equipped With Skids

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    https://yetl.yabesh.ir/yetl1/handle/yetl/91546
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    contributor authorChing-U Ip
    date accessioned2017-05-08T23:05:42Z
    date available2017-05-08T23:05:42Z
    date copyrightAugust, 1962
    date issued1962
    identifier issn1087-1357
    identifier otherJMSEFK-27464#301_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/91546
    description abstractEquations of motion of the airplane subject to the influence of cross wind, rudder steering, and drag chute, during runout, are developed which would be valid even when the direction-of-travel angle and the yaw angle are large. A procedure of synthesizing the runout path step by step explicitly is presented. A flight vehicle capable of orbiting around the earth usually does not have ground steering capability because its weight has to be held to a minimum. This study will enable a designer to determine whether or not the vehicle will have inherent stability to land on a runway.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRunout Path of an Airplane Equipped With Skids
    typeJournal Paper
    journal volume84
    journal issue3
    journal titleJournal of Manufacturing Science and Engineering
    identifier doi10.1115/1.3667481
    journal fristpage301
    journal lastpage306
    identifier eissn1528-8935
    keywordsAircraft
    keywordsVehicles
    keywordsTravel
    keywordsWind
    keywordsYaw
    keywordsFlight
    keywordsWeight (Mass)
    keywordsStability
    keywordsDrag (Fluid dynamics) AND Equations of motion
    treeJournal of Manufacturing Science and Engineering:;1962:;volume( 084 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian