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    First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop

    Wood, Richard M. | NTRS | 1999
    This publication is a compilation of documents presented at the First NASA/Industry High Speed Research Configuration Aerodynamics Workshop ...
    Schlagwörter: Aerodynamics

    First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop

    Wood, Richard M. | NTRS | 1999
    This publication is a compilation of documents presented at the First NASA/Industry High Speed Research Configuration Aerodynamics Workshop ...
    Schlagwörter: Aerodynamics

    First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop

    NTIS | 1999
    This publication is a compilation of documents presented at the First NASA/Industry High Speed Research Configuration Aerodynamics Workshop ...
    Verlag: National Aeronautics and Space Administration, Hampton, VA. Langley Research Center
    Schlagwörter: Aerodynamics

    First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop

    Wood, Richard M. | NTRS | 1999
    This publication is a compilation of documents presented at the First NASA Industry High Speed Research Configuration Aerodynamics Workshop ...

    First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop, Part 1

    NTIS | 1999
    This publication is a compilation of documents presented at the First NASA/Industry High Speed Research Configuration Aerodynamics Workshop ...
    Verlag: National Aeronautics and Space Administration, Hampton, VA. Langley Research Center
    Schlagwörter: Aerodynamics

    First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop, Pt. 2

    NTIS | 1999
    This publication is a compilation of documents presented at the First NASA Industry High Speed Research Configuration Aerodynamics Workshop ...
    Verlag: National Aeronautics and Space Administration, Hampton, VA. Langley Research Center
    Schlagwörter: Aerodynamics , High speed

    High-Speed Research Project

    Bharadvaj, Bala / Fischer, Mike / Joslin, Ronald D. et al. | NTRS | 1999
    Schlagwörter: Aerodynamics

    Configuration Aerodynamics: Past - Present - Future

    Wood, Richard M. / Agrawal, Shreekant / Bencze, Daniel P. et al. | NTRS | 1999
    The Configuration Aerodynamics (CA) element of the High Speed Research (HSR) program is managed by a joint NASA and Industry team, referred ...
    Schlagwörter: Aerodynamics

    Experimental Results of the 2.7% Reference H Nacelle Airframe Interference High Speed Civil Transport Model

    Cappuccio, Gelsomina | NTRS | 1999
    ) Nacelle Airframe Interference (NAI) High Speed Civil Transport (HSCT) model. NASA Ames did the experiment with the cooperation and assistance of ...
    Schlagwörter: Aerodynamics

    High Speed Civil Transport (HSCT) Isolated Nacelle Transonic Boattail Drag Study and Results Using Computational Fluid Dynamics (CFD)

    Midea, Anthony C. / Austin, Thomas / Pao, S. Paul et al. | NTRS | 1999
    Nozzle boattail drag is significant for the High Speed Civil Transport (HSCT) and can be as high as 25% of the overall propulsion system ...
    Schlagwörter: Aerodynamics

    Simulated Inlet Unstart and Nacelle/Diverter Effects for the Boeing Reference H Configuration

    Cliff, Susan E. / Baker, Timothy J. / Thomas, Scott D. et al. | NTRS | 1999
    The Boeing Reference H configuration was tested in the NASA Ames 9x7 Supersonic Wind Tunnel. A simulated unstarted inlet was evaluated as ...
    Schlagwörter: Aerodynamics

    The Application of the NFW Design Philosophy to the HSR Arrow Wing Configuration

    Bauer, Steven X. S. / Krist, Steven E. | NTRS | 1999
    not violating any structural constraints) was developed and the resulting geometries were analyzed and compared to a baseline configuration ...

    Supersonic Aerodynamic Design Improvements of an Arrow-Wing HSCT Configuration Using Nonlinear Point Design Methods

    Unger, Eric R. / Hager, James O. / Agrawal, Shreekant | NTRS | 1999
    -Speed Research (HSR) program. The baseline for these optimization efforts has been the M2.4-7A configuration which represents an arrow-wing ...

    Initial Results of Reynolds Number Testing at LaRC's NTF Using the 2.2% Reference H Model

    Owens, Lewis R., Jr. / Wahls, Richard A. / Hamner, Marvine | NTRS | 1999
    . A wind tunnel database utilizing a 2.2% scale Reference H model in NASA Langley Research Centers National Transonic Facility is being ...
    Schlagwörter: Aerodynamics

    HSCT Ref-H Transonic Flap Data Base: Wind-Tunnel Test and Comparison with Theory

    Vijgen, Paul M. | NTRS | 1999
    Schlagwörter: Aerodynamics

    Technology Integration Overview

    Coen, Peter G. | NTRS | 1999
    Schlagwörter: Aerodynamics

    A Computational/Experimental Study of Two Optimized Supersonic Transport Designs and the Reference H Baseline

    Cliff, Susan E. / Baker, Timothy J. / Hicks, Raymond M. et al. | NTRS | 1999
    designed baseline configuration. One optimized configuration, designated Ames 7-04, was designed at NASA Ames Research Center using an Euler flow ...

    High Reynolds Number Effects on HSCT Stability and Control Characteristics

    Elzey, Michael B. / Owens, Lewis R., Jr. / Wahls, Richard A. et al. | NTRS | 1999
    number on the total airplane configuration, horizontal and vertical tail effectiveness, forebody chine performance, rudder control and model ...

    Potential for Sonic Boom Reduction of the Boeing HSCT

    Haglund, George T. | NTRS | 1999
    minimize the effect on the configuration performance. This work was a joint NASA/Industry effort, utilizing the respective strengths of team ...
    Schlagwörter: Aerodynamics

    A PTC Optimization and Control Surface Interference Study HSR Airframe Technical Review

    Hicks, Raymond / Cliff, Susan / Rimlinger, Mark et al. | NTRS | 1999
    configuration without nacelles and diverters. This analysis is followed by three optimization studies using canard and tail incidence as design ...
    Schlagwörter: Aerodynamics

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