Search Results - Follador, Roberto Da Cunha

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  1. 1
    Knowledge Management Patterns Model for a Flight Test Environment

    Knowledge Management Patterns Model for a Flight Test Environment by Follador, Roberto Da Cunha, Trabasso, Luís Gonzaga

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  2. 2
    Comparison of in-Flight Measured and Computed Aeroelastic Damping: Modal Identification Procedures and Modeling Approaches

    Comparison of in-Flight Measured and Computed Aeroelastic Damping: Modal Identification Procedures and Modeling Approaches by Follador, Roberto Da Cunha, Souza, Carlos Eduardo de, Marto, Adolfo Gomes, Silva, Roberto Gil Annes da, Góes, Luis Carlos Sandoval

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  3. 3
    Experimental results of a Mach 10 conical-flow derived waverider to 14-X hypersonic aerospace vehicle

    Experimental results of a Mach 10 conical-flow derived waverider to 14-X hypersonic aerospace vehicle by Rolim, Tiago Cavalcanti, Toro, Paulo Gilberto de Paula, Minucci, Marco Antonio Sala, Oliveira, Antônio de Carlos de, Follador, Roberto da Cunha

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  4. 4
    Knowledge Management Patterns Model for a Flight Test Environment

    Knowledge Management Patterns Model for a Flight Test Environment by Roberto da Cunha Follador, Luís Gonzaga Trabasso

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  5. 5
    Comparison of In-Flight Measured and Computed Aeroelastic Damping: Modal Identification Procedures and Modeling Approaches

    Comparison of In-Flight Measured and Computed Aeroelastic Damping: Modal Identification Procedures and Modeling Approaches by Roberto da Cunha Follador, Carlos Eduardo de Souza, Adolfo Gomes Marto, Roberto Gil Annes da Silva, Luis Carlos Sandoval Góes

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  6. 6
    EXPERIMENTAL RESULTS OF A MACH 10 CONICAL-FLOW DERIVED WAVERIDER TO 14-X HYPERSONIC AEROSPACE VEHICLE. doi: 10.5028/jatm.2011.03027510

    EXPERIMENTAL RESULTS OF A MACH 10 CONICAL-FLOW DERIVED WAVERIDER TO 14-X HYPERSONIC AEROSPACE VEHICLE. doi: 10.5028/jatm.2011.03027510 by Tiago Cavalcanti Rolim, Paulo Gilberto de Paula Toro, Marco Antonio Sala Minucci, Antônio Carlos de Oliveira, Roberto da Cunha Follador

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  7. 7
    Experimental results of a Mach 10 conical-flow derived waverider to 14-X hypersonic airspace vehicle

    Experimental results of a Mach 10 conical-flow derived waverider to 14-X hypersonic airspace vehicle by Rolim, Tiago Cavalcanti, Toro, Paulo Gilberto de Paula, Minucci, Marco Antonio Sala, Oliveira, Antônio de Carlos de, Follador, Roberto da Cunha

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