1–20 von 31 Ergebnissen
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    Aerodynamics design of convergent-divergent nozzles

    REBOLO, R. / ARREDONDO, P. / MATESANZ, A. et al. | AIAA | 1993

    Performance enhancement for a missile in the presence of saturating actuators

    Rodriguez, Armando A. / Cloutier, James R. | AIAA | 1996

    Integration of hypersonic aerothermodynamics design methods

    Lopez-Reig, J. / Rebolo, R. / Matesanz, A. et al. | AIAA | 1996

    Testing of an advanced liquid hydrogen turbopump

    Grabowski, R. / Chapman, L. / Crease, G. et al. | AIAA | 2000

    Experimental and Numerical Study of a Dual-mode Scramjet Combustor

    C. Goyne / C. Rodriguez / R. Krauss et al. | AIAA | 2006

    ISS Crew Quarters On-Orbit Performance and Sustaining Activities

    Schlesinger, Thilini / Rodriguez, Branelle R. / Borrego, Melissa | AIAA | 2013

    Mars Science Laboratory Heat Shield Instrumentation and Arc Jet Characterization

    Bose, Deepak / Santos, Jose A. / Rodriguez, Erika et al. | AIAA | 2013

    Extraction of Turbofan Combustion Noise Spectra Using a combined Coherence-Beamforming Technique

    Rodriguez-Garcia, Paul / Holland, Keith R. / Tester, Brian J. | AIAA | 2014

    Optimized Off-Design Performance of Flexible Wings with Continuous Trailing-Edge Flaps

    Rodriguez, David L. / Aftosmis, Michael J. / Nemec, Marian et al. | AIAA | 2015

    Impact of Oxygen Enrichment on the Performance of Heat-Recirculating Micro-Scale Combustors

    Yelvington, Paul E. / Rodriguez, Christian O. / Lasko, Thomas M. et al. | AIAA | 2015

    Optimization of Flexible Wings with Distributed Flaps at Off-Design Conditions

    Rodriguez, David L. / Aftosmis, Michael J. / Nemec, Marian et al. | AIAA | 2016