41–60 von 61 Ergebnissen
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    Summary of the 2008 NASA Fundamental Aeronautics Program Sonic Boom Prediction Workshop

    Park, Michael A. / Aftosmis, Michael J. / Campbell, Richard L. et al. | NTRS | 2013

    Summary of the 2008 NASA Fundamental Aeronautics Program Sonic Boom Prediction Workshop

    Park, Michael A. / Aftosmis, Michael J. / Campbell, Richard L. et al. | AIAA | 2014

    Computational Component Build-up for the X-57 Maxwell Distributed Electric Propulsion Aircraft (AIAA 2018-1275)

    Deere, Karen A. / Viken, Sally / Carter, Melissa B. et al. | British Library Conference Proceedings | 2018

    X-59 Sonic Boom Test Results from the NASA Glenn 8- by 6-Foot Supersonic Wind Tunnel

    Durston, Donald A. / Wolter, John D. / Shea, Patrick et al. | AIAA | 2023

      X-59 Sonic Boom Test Results from the NASA Glenn 8- By 6-Foot Supersonic Wind Tunnel

      Durston, Donald A. / Wolter, John D. / Shea, Patrick et al. | TIBKAT | 2023

    Design and Testing of a Blended Wing Body With Boundary Layer Ingestion Nacelles at High Reynolds Numbers

    Campbell, Richard L. / Carter, Melissa B. / Pendergraft, Odis C., Jr. et al. | NTRS | 2005

    Comparison of Aero-Propulsive Performance Predictions for Distributed Propulsion Configurations (AIAA 2017-0209)

    Borer, Nicholas K. / Derlaga, Joseph M. / Deere, Karen A. et al. | British Library Conference Proceedings | 2017

    Experimental Evaluation of Inlet Distortion on an Ejector Powered Hybrid Wing Body at Take-off and Landing Conditions (Invited) (AIAA 2016-0010)

    Carter, Melissa B. / Shea, Patrick R. / Flamm, Jeff D. et al. | British Library Conference Proceedings | 2016

    Designing and Testing a Blended Wing Body with Boundary Layer Ingestion Nacelles

    Carter, Melissa B. / Campbell, Richard L. / Pendergraft, Odis C. et al. | NTRS | 2006

    Enhancements to the FAST-MAC Circulation Control Model and Recent High-Reynolds Number Testing in the National Transonic Facility

    Milholen, William E. / Jones, Gregory S. / Chan, David T. et al. | AIAA | 2013

    Development of the Circulation Control Flow Scheme used in the NTF Semi-Span FAST-MAC Model

    Jones, Gregory S. / Milholen, William E. / Chan, David T. et al. | AIAA | 2013

      Development of the Circulation Control Flow Scheme Used in the NTF Semi-Span FAST-MAC Model

      Jones, Gregory S. / Milholen, William E., II / Chan, David T. et al. | NTRS | 2013

    Nozzle Plume/Shock Interaction Sonic Boom Test Results from the NASA Ames 9- by 7-Foot Supersonic Wind Tunnel

    Durston, Donald A. / Cliff, Susan E. / Denison, Marie et al. | AIAA | 2017

    Computational Evaluation of Inlet Distortion on an Ejector Powered Hybrid Wing Body at Takeoff and Landing Conditions

    Tompkins, Daniel M. / Sexton, Matthew R. / Mugica, Edward A. et al. | NTRS | 2016

    NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration (Invited) (AIAA 2016-0262)

    Garcia, Joseph A. / Melton, John / Schuh, Michael J. et al. | British Library Conference Proceedings | 2016

    Nozzle Plume/Shock Interaction Sonic Boom Test Results from the NASA Ames 9- by 7-Foot Supersonic Wind Tunnel (AIAA 2017-0041)

    Durston, Donald A. / Cliff, Susan E. / Denison, Marie et al. | British Library Conference Proceedings | 2017

    NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration (Invited)

    Garcia, Joseph A. / Melton, John / Schuh, Michael J. et al. | AIAA | 2016

    NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration

    Garcia, Joseph A. / Melton, John E. / Schuh, Michael et al. | NTRS | 2016

    NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration

    Garcia, Joseph A. / Melton, John E. / Schuh, Michael et al. | NTRS | 2016