@prefix dcat: <http://www.w3.org/ns/dcat#> .
@prefix dct: <http://purl.org/dc/terms/> .
@prefix foaf: <http://xmlns.com/foaf/0.1/> .
@prefix vcard: <http://www.w3.org/2006/vcard/ns#> .
@prefix xsd: <http://www.w3.org/2001/XMLSchema#> .

<https://data.amerigeoss.org/dataset/49b8773f-c7fc-4efc-88f6-e59de3901c71> a dcat:Dataset ;
    dct:description """The proposed research program aims at developing a variable-fidelity
software tool set for aeroservothermoelastic-propulsive (ASTE-P)
modeling that can be routinely applied to the design of aerospace
vehicles. The tool set can be applied to conventional vehicle types as
well as hypersonic vehicles. The major issues involved in ASTE-P
modeling and simulation will be significantly and extensively
investigated in this project, which include full coupling between
fluid/structure/control dynamics, the aeroservothermoelastic-propulsive
instability, the viscous/turbulent effects, shock and shock-boundary
layer interaction, as well as the large unsteady and highly nonlinear
aerothermal dynamic loading on structure of vehicles. The interface of
the structure/control surface dynamic vibration modes with flows will be
modeled using particle-based material point method (MPM) in an
integrated dynamic fluid-structure interaction environment.  The MPM is
essentially a particle-based method which avoids dealing with the
time-varying mesh distortions and boundary variations due to
structure/control surface deformations and/or motions (i.e. wing
flutters, FCS/structural mode interaction, PSD turbulence response),
thus being significantly more robust and computationally efficient than
the traditional finite element methods that must utilize moving-boundary
and mesh-regeneration. Phase I will build and demonstrate the initial
capability; the end software in Phase II will be fully capable of ASTE-P
analysis and evaluation for aerospace vehicles.""" ;
    dct:identifier "49b8773f-c7fc-4efc-88f6-e59de3901c71" ;
    dct:issued "2025-11-29T17:48:41.773157"^^xsd:dateTime ;
    dct:modified "2025-11-29T17:48:41.773161"^^xsd:dateTime ;
    dct:publisher <https://data.amerigeoss.org/organization/727dbdd5-3f98-4ac0-9d28-5e344558139b> ;
    dct:title "Integrated Variable-Fidelity Tool Set For Modeling and Simulation of Aeroservothermoelasticity -Propulsion (ASTE-P) Effects For Aerospace Vehicles Ranging From Subsonic to Hypersonic Flight, Phase I" ;
    dcat:contactPoint [ a vcard:Organization ;
            vcard:fn "TECHPORT SUPPORT" ;
            vcard:hasEmail <mailto:hq-techport@mail.nasa.gov> ] ;
    dcat:distribution <https://data.amerigeoss.org/dataset/49b8773f-c7fc-4efc-88f6-e59de3901c71/resource/355c5d17-4695-4fec-975f-f5cea308018b>,
        <https://data.amerigeoss.org/dataset/49b8773f-c7fc-4efc-88f6-e59de3901c71/resource/3e1eb42e-f6f1-416c-8c02-602b189ca6ce>,
        <https://data.amerigeoss.org/dataset/49b8773f-c7fc-4efc-88f6-e59de3901c71/resource/a06e2743-35dd-4149-a435-be9a27be2c89>,
        <https://data.amerigeoss.org/dataset/49b8773f-c7fc-4efc-88f6-e59de3901c71/resource/d0272611-3b84-4089-addb-5963297bb1ac> ;
    dcat:keyword "amerigeo",
        "amerigeoss",
        "ckan",
        "geo",
        "geoss",
        "national",
        "north-america",
        "united-states" .

<https://data.amerigeoss.org/dataset/49b8773f-c7fc-4efc-88f6-e59de3901c71/resource/355c5d17-4695-4fec-975f-f5cea308018b> a dcat:Distribution ;
    dct:description "Techport Project XML Metadata" ;
    dct:format "HTML" ;
    dct:issued "2018-08-01T17:07:22.058073"^^xsd:dateTime ;
    dct:modified "2025-11-29T17:48:41.766845"^^xsd:dateTime ;
    dct:title "Integrated Variable-Fidelity Tool Set For Modeling and Simulation of Aeroservothermoelasticity -Propulsion (ASTE-P) Effects For Aerospace Vehicles Ranging From Subsonic to Hypersonic Flight, Phase I" ;
    dcat:accessURL <https://techport.nasa.gov/api/projects/6337.xml> ;
    dcat:mediaType "text/html" .

<https://data.amerigeoss.org/dataset/49b8773f-c7fc-4efc-88f6-e59de3901c71/resource/3e1eb42e-f6f1-416c-8c02-602b189ca6ce> a dcat:Distribution ;
    dct:description "Techport Project JSON Metadata" ;
    dct:format "HTML" ;
    dct:issued "2018-08-01T17:07:22.058069"^^xsd:dateTime ;
    dct:modified "2025-11-29T17:48:41.766444"^^xsd:dateTime ;
    dct:title "Integrated Variable-Fidelity Tool Set For Modeling and Simulation of Aeroservothermoelasticity -Propulsion (ASTE-P) Effects For Aerospace Vehicles Ranging From Subsonic to Hypersonic Flight, Phase I" ;
    dcat:accessURL <https://techport.nasa.gov/api/projects/6337> ;
    dcat:mediaType "text/html" .

<https://data.amerigeoss.org/dataset/49b8773f-c7fc-4efc-88f6-e59de3901c71/resource/a06e2743-35dd-4149-a435-be9a27be2c89> a dcat:Distribution ;
    dct:description "Techport Project Page" ;
    dct:format "HTML" ;
    dct:issued "2018-08-01T17:07:22.058050"^^xsd:dateTime ;
    dct:modified "2025-11-29T17:48:41.766018"^^xsd:dateTime ;
    dct:title "Integrated Variable-Fidelity Tool Set For Modeling and Simulation of Aeroservothermoelasticity -Propulsion (ASTE-P) Effects For Aerospace Vehicles Ranging From Subsonic to Hypersonic Flight, Phase I" ;
    dcat:accessURL <https://techport.nasa.gov/view/6337> ;
    dcat:mediaType "text/html" .

<https://data.amerigeoss.org/dataset/49b8773f-c7fc-4efc-88f6-e59de3901c71/resource/d0272611-3b84-4089-addb-5963297bb1ac> a dcat:Distribution ;
    dct:description "Techport Project PDF Export" ;
    dct:format "HTML" ;
    dct:issued "2018-08-01T17:07:22.058076"^^xsd:dateTime ;
    dct:modified "2025-11-29T17:48:41.767223"^^xsd:dateTime ;
    dct:title "Integrated Variable-Fidelity Tool Set For Modeling and Simulation of Aeroservothermoelasticity -Propulsion (ASTE-P) Effects For Aerospace Vehicles Ranging From Subsonic to Hypersonic Flight, Phase I" ;
    dcat:accessURL <https://techport.nasa.gov/datasheet/6337> ;
    dcat:mediaType "text/html" .

<https://data.amerigeoss.org/organization/727dbdd5-3f98-4ac0-9d28-5e344558139b> a foaf:Agent ;
    foaf:name "US Migrating" .