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de Oliveira, Paulo Henriques Iscold Andrade
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Mathematical Modeling for Optimization of Competition Sailplane Flight: a Preliminary Approach
- Technical Paper
- 2003-01-3622
- DOI: https://doi.org/10.4271/2003-01-3622
Published
2003-11-18
by SAE International in United States
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Light Aircraft Instrumentation to Determine Performance, Stability and Control Characteristics in Flight Tests
- Technical Paper
- 2004-01-3474
- DOI: https://doi.org/10.4271/2004-01-3474
Published
2004-11-16
by SAE International in United States
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Flight Path Optimization for Competition Sailplanes through State Variables Parameterization
- Technical Paper
- 2004-01-3472
- DOI: https://doi.org/10.4271/2004-01-3472
Published
2004-11-16
by SAE International in United States
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Development of a Light Aircraft Flight Test Equipment
- Technical Paper
- 2005-01-4081
- DOI: https://doi.org/10.4271/2005-01-4081
Published
2005-11-22
by SAE International in United States
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Crashworthy Composite Fuselage Section Concept for Next Generation General Aviation
- Technical Paper
- 2005-01-4011
- DOI: https://doi.org/10.4271/2005-01-4011
Published
2005-11-22
by SAE International in United States
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Aspects of the Application of a Three Dimensional Panel Method Tool in the Design of a Light Aircraft
- Technical Paper
- 2005-01-4161
- DOI: https://doi.org/10.4271/2005-01-4161
Published
2005-11-22
by SAE International in United States
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A Review of Finite Element Simulation of Aircraft Crashworthiness
- Technical Paper
- 2005-01-4012
- DOI: https://doi.org/10.4271/2005-01-4012
Published
2005-11-22
by SAE International in United States
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Sub-optimal control laws for minimization of take-off distance for aircrafts
- Technical Paper
- 2006-01-2865
- DOI: https://doi.org/10.4271/2006-01-2865
Published
2006-11-21
by SAE International in United States
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Development of an UAV Aircraft for General Purposes
- Technical Paper
- 2006-01-2777
- DOI: https://doi.org/10.4271/2006-01-2777
Published
2006-11-21
by SAE International in United States
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A Fast Aerodynamic Procedure for a Complete Aircraft Design Using the Know Airfoil Characteristics
- Technical Paper
- 2006-01-2818
- DOI: https://doi.org/10.4271/2006-01-2818
Published
2006-11-21
by SAE International in United States