Dynamics of a parachute panel on opening
Conclusions Tensile forces in the panel of a parachute on opening are approximately double those in the same panel for the same pressure-gradient amplitude. It is therefore necessary to compute the cell strength of a parachute canopy proceeding from dynamic load levels.It is apparent that the thread...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Vasilo'chenko, A. G. [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
1985 |
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| Schlagwörter: |
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| Anmerkung: |
© Plenum Publishing Corporation 1985 |
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| Übergeordnetes Werk: |
Enthalten in: Mechanics of composite materials - Kluwer Academic Publishers-Plenum Publishers, 1980, 21(1985), 3 vom: Mai, Seite 316-322 |
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| Übergeordnetes Werk: |
volume:21 ; year:1985 ; number:3 ; month:05 ; pages:316-322 |
| Links: |
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| DOI / URN: |
10.1007/BF00611617 |
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| Katalog-ID: |
OLC2081277263 |
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| 520 | |a Conclusions Tensile forces in the panel of a parachute on opening are approximately double those in the same panel for the same pressure-gradient amplitude. It is therefore necessary to compute the cell strength of a parachute canopy proceeding from dynamic load levels.It is apparent that the threads of the base and weft must be placed at an angle$$\mathop \mu \limits^ \circ $$= 45° with respect to the boundaries that surround it (strips) to reduce the overall level of the stress-strain state of a panel subjected to dynamic effects and to load the fabric more uniformly.It is established that the elongation coefficient ξ of the panel exerts a weak influence on the dynamic-effect factor k* of the system; at the same time, however, the cut of the fabric has a significant effect on its magnitude. | ||
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10.1007/BF00611617 doi (DE-627)OLC2081277263 (DE-He213)BF00611617-p DE-627 ger DE-627 rakwb eng 540 VZ Vasilo'chenko, A. G. verfasserin aut Dynamics of a parachute panel on opening 1985 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Plenum Publishing Corporation 1985 Conclusions Tensile forces in the panel of a parachute on opening are approximately double those in the same panel for the same pressure-gradient amplitude. It is therefore necessary to compute the cell strength of a parachute canopy proceeding from dynamic load levels.It is apparent that the threads of the base and weft must be placed at an angle$$\mathop \mu \limits^ \circ $$= 45° with respect to the boundaries that surround it (strips) to reduce the overall level of the stress-strain state of a panel subjected to dynamic effects and to load the fabric more uniformly.It is established that the elongation coefficient ξ of the panel exerts a weak influence on the dynamic-effect factor k* of the system; at the same time, however, the cut of the fabric has a significant effect on its magnitude. Dynamic Load Dynamic Effect Load Level Tensile Force Weak Influence Ponomarev, A. T. aut Enthalten in Mechanics of composite materials Kluwer Academic Publishers-Plenum Publishers, 1980 21(1985), 3 vom: Mai, Seite 316-322 (DE-627)130525332 (DE-600)771508-0 (DE-576)9130525330 0191-5665 nnns volume:21 year:1985 number:3 month:05 pages:316-322 https://doi.org/10.1007/BF00611617 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-CHE SSG-OLC-PHA GBV_ILN_70 GBV_ILN_4046 AR 21 1985 3 05 316-322 |
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10.1007/BF00611617 doi (DE-627)OLC2081277263 (DE-He213)BF00611617-p DE-627 ger DE-627 rakwb eng 540 VZ Vasilo'chenko, A. G. verfasserin aut Dynamics of a parachute panel on opening 1985 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Plenum Publishing Corporation 1985 Conclusions Tensile forces in the panel of a parachute on opening are approximately double those in the same panel for the same pressure-gradient amplitude. It is therefore necessary to compute the cell strength of a parachute canopy proceeding from dynamic load levels.It is apparent that the threads of the base and weft must be placed at an angle$$\mathop \mu \limits^ \circ $$= 45° with respect to the boundaries that surround it (strips) to reduce the overall level of the stress-strain state of a panel subjected to dynamic effects and to load the fabric more uniformly.It is established that the elongation coefficient ξ of the panel exerts a weak influence on the dynamic-effect factor k* of the system; at the same time, however, the cut of the fabric has a significant effect on its magnitude. Dynamic Load Dynamic Effect Load Level Tensile Force Weak Influence Ponomarev, A. T. aut Enthalten in Mechanics of composite materials Kluwer Academic Publishers-Plenum Publishers, 1980 21(1985), 3 vom: Mai, Seite 316-322 (DE-627)130525332 (DE-600)771508-0 (DE-576)9130525330 0191-5665 nnns volume:21 year:1985 number:3 month:05 pages:316-322 https://doi.org/10.1007/BF00611617 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-CHE SSG-OLC-PHA GBV_ILN_70 GBV_ILN_4046 AR 21 1985 3 05 316-322 |
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10.1007/BF00611617 doi (DE-627)OLC2081277263 (DE-He213)BF00611617-p DE-627 ger DE-627 rakwb eng 540 VZ Vasilo'chenko, A. G. verfasserin aut Dynamics of a parachute panel on opening 1985 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Plenum Publishing Corporation 1985 Conclusions Tensile forces in the panel of a parachute on opening are approximately double those in the same panel for the same pressure-gradient amplitude. It is therefore necessary to compute the cell strength of a parachute canopy proceeding from dynamic load levels.It is apparent that the threads of the base and weft must be placed at an angle$$\mathop \mu \limits^ \circ $$= 45° with respect to the boundaries that surround it (strips) to reduce the overall level of the stress-strain state of a panel subjected to dynamic effects and to load the fabric more uniformly.It is established that the elongation coefficient ξ of the panel exerts a weak influence on the dynamic-effect factor k* of the system; at the same time, however, the cut of the fabric has a significant effect on its magnitude. Dynamic Load Dynamic Effect Load Level Tensile Force Weak Influence Ponomarev, A. T. aut Enthalten in Mechanics of composite materials Kluwer Academic Publishers-Plenum Publishers, 1980 21(1985), 3 vom: Mai, Seite 316-322 (DE-627)130525332 (DE-600)771508-0 (DE-576)9130525330 0191-5665 nnns volume:21 year:1985 number:3 month:05 pages:316-322 https://doi.org/10.1007/BF00611617 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-CHE SSG-OLC-PHA GBV_ILN_70 GBV_ILN_4046 AR 21 1985 3 05 316-322 |
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10.1007/BF00611617 doi (DE-627)OLC2081277263 (DE-He213)BF00611617-p DE-627 ger DE-627 rakwb eng 540 VZ Vasilo'chenko, A. G. verfasserin aut Dynamics of a parachute panel on opening 1985 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Plenum Publishing Corporation 1985 Conclusions Tensile forces in the panel of a parachute on opening are approximately double those in the same panel for the same pressure-gradient amplitude. It is therefore necessary to compute the cell strength of a parachute canopy proceeding from dynamic load levels.It is apparent that the threads of the base and weft must be placed at an angle$$\mathop \mu \limits^ \circ $$= 45° with respect to the boundaries that surround it (strips) to reduce the overall level of the stress-strain state of a panel subjected to dynamic effects and to load the fabric more uniformly.It is established that the elongation coefficient ξ of the panel exerts a weak influence on the dynamic-effect factor k* of the system; at the same time, however, the cut of the fabric has a significant effect on its magnitude. Dynamic Load Dynamic Effect Load Level Tensile Force Weak Influence Ponomarev, A. T. aut Enthalten in Mechanics of composite materials Kluwer Academic Publishers-Plenum Publishers, 1980 21(1985), 3 vom: Mai, Seite 316-322 (DE-627)130525332 (DE-600)771508-0 (DE-576)9130525330 0191-5665 nnns volume:21 year:1985 number:3 month:05 pages:316-322 https://doi.org/10.1007/BF00611617 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-CHE SSG-OLC-PHA GBV_ILN_70 GBV_ILN_4046 AR 21 1985 3 05 316-322 |
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10.1007/BF00611617 doi (DE-627)OLC2081277263 (DE-He213)BF00611617-p DE-627 ger DE-627 rakwb eng 540 VZ Vasilo'chenko, A. G. verfasserin aut Dynamics of a parachute panel on opening 1985 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Plenum Publishing Corporation 1985 Conclusions Tensile forces in the panel of a parachute on opening are approximately double those in the same panel for the same pressure-gradient amplitude. It is therefore necessary to compute the cell strength of a parachute canopy proceeding from dynamic load levels.It is apparent that the threads of the base and weft must be placed at an angle$$\mathop \mu \limits^ \circ $$= 45° with respect to the boundaries that surround it (strips) to reduce the overall level of the stress-strain state of a panel subjected to dynamic effects and to load the fabric more uniformly.It is established that the elongation coefficient ξ of the panel exerts a weak influence on the dynamic-effect factor k* of the system; at the same time, however, the cut of the fabric has a significant effect on its magnitude. Dynamic Load Dynamic Effect Load Level Tensile Force Weak Influence Ponomarev, A. T. aut Enthalten in Mechanics of composite materials Kluwer Academic Publishers-Plenum Publishers, 1980 21(1985), 3 vom: Mai, Seite 316-322 (DE-627)130525332 (DE-600)771508-0 (DE-576)9130525330 0191-5665 nnns volume:21 year:1985 number:3 month:05 pages:316-322 https://doi.org/10.1007/BF00611617 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-CHE SSG-OLC-PHA GBV_ILN_70 GBV_ILN_4046 AR 21 1985 3 05 316-322 |
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Conclusions Tensile forces in the panel of a parachute on opening are approximately double those in the same panel for the same pressure-gradient amplitude. It is therefore necessary to compute the cell strength of a parachute canopy proceeding from dynamic load levels.It is apparent that the threads of the base and weft must be placed at an angle$$\mathop \mu \limits^ \circ $$= 45° with respect to the boundaries that surround it (strips) to reduce the overall level of the stress-strain state of a panel subjected to dynamic effects and to load the fabric more uniformly.It is established that the elongation coefficient ξ of the panel exerts a weak influence on the dynamic-effect factor k* of the system; at the same time, however, the cut of the fabric has a significant effect on its magnitude. © Plenum Publishing Corporation 1985 |
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Conclusions Tensile forces in the panel of a parachute on opening are approximately double those in the same panel for the same pressure-gradient amplitude. It is therefore necessary to compute the cell strength of a parachute canopy proceeding from dynamic load levels.It is apparent that the threads of the base and weft must be placed at an angle$$\mathop \mu \limits^ \circ $$= 45° with respect to the boundaries that surround it (strips) to reduce the overall level of the stress-strain state of a panel subjected to dynamic effects and to load the fabric more uniformly.It is established that the elongation coefficient ξ of the panel exerts a weak influence on the dynamic-effect factor k* of the system; at the same time, however, the cut of the fabric has a significant effect on its magnitude. © Plenum Publishing Corporation 1985 |
| abstract_unstemmed |
Conclusions Tensile forces in the panel of a parachute on opening are approximately double those in the same panel for the same pressure-gradient amplitude. It is therefore necessary to compute the cell strength of a parachute canopy proceeding from dynamic load levels.It is apparent that the threads of the base and weft must be placed at an angle$$\mathop \mu \limits^ \circ $$= 45° with respect to the boundaries that surround it (strips) to reduce the overall level of the stress-strain state of a panel subjected to dynamic effects and to load the fabric more uniformly.It is established that the elongation coefficient ξ of the panel exerts a weak influence on the dynamic-effect factor k* of the system; at the same time, however, the cut of the fabric has a significant effect on its magnitude. © Plenum Publishing Corporation 1985 |
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G.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Dynamics of a parachute panel on opening</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">1985</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">ohne Hilfsmittel zu benutzen</subfield><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Band</subfield><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© Plenum Publishing Corporation 1985</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Conclusions Tensile forces in the panel of a parachute on opening are approximately double those in the same panel for the same pressure-gradient amplitude. It is therefore necessary to compute the cell strength of a parachute canopy proceeding from dynamic load levels.It is apparent that the threads of the base and weft must be placed at an angle$$\mathop \mu \limits^ \circ $$= 45° with respect to the boundaries that surround it (strips) to reduce the overall level of the stress-strain state of a panel subjected to dynamic effects and to load the fabric more uniformly.It is established that the elongation coefficient ξ of the panel exerts a weak influence on the dynamic-effect factor k* of the system; at the same time, however, the cut of the fabric has a significant effect on its magnitude.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Dynamic Load</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Dynamic Effect</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Load Level</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Tensile Force</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Weak Influence</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Ponomarev, A. T.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Mechanics of composite materials</subfield><subfield code="d">Kluwer Academic Publishers-Plenum Publishers, 1980</subfield><subfield code="g">21(1985), 3 vom: Mai, Seite 316-322</subfield><subfield code="w">(DE-627)130525332</subfield><subfield code="w">(DE-600)771508-0</subfield><subfield code="w">(DE-576)9130525330</subfield><subfield code="x">0191-5665</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:21</subfield><subfield code="g">year:1985</subfield><subfield code="g">number:3</subfield><subfield code="g">month:05</subfield><subfield code="g">pages:316-322</subfield></datafield><datafield tag="856" ind1="4" ind2="1"><subfield code="u">https://doi.org/10.1007/BF00611617</subfield><subfield code="z">lizenzpflichtig</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_OLC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-TEC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-CHE</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-PHA</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4046</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">21</subfield><subfield code="j">1985</subfield><subfield code="e">3</subfield><subfield code="c">05</subfield><subfield code="h">316-322</subfield></datafield></record></collection>
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