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    Wind-Tunnel Studies at Subsonic and Transonic Speeds of a Multiple-Mission Variable-Wing- Sweep Airplane Configuration

    W. J. Alford / W. P. Henderson / A. A. Luoma | NTIS | 1959
    Schlagwörter: Aircraft configuration , Aircraft , Fuselage

    New Concepts and Perspectives on Micro-Rotorcraft and Small Autonomous Rotary-Wing Vehicles

    L. A. Young / E. W. Aiken / J. L. Johnson et al. | NTIS | 2002
    Schlagwörter: Aircraft , Rotary wing aircraft , Aircraft design , Tilt rotor aircraft , Tandem twin-fuselage tiltrotors

    Flight Measurements of Lifting Pressures for a Thin Low-Aspect-Ratio Wing at Subsonic, Transonic, and Low Supersonic Speeds

    T. A. Byrdsong | NTIS | 1977
    Schlagwörter: Aircraft , Aircraft maneuvers , Wing-fuselage stores

    Active control of helicopter vibration

    Pearson, J.T. / Goodall, R.M. / Lyndon, I. | Tema Archiv | 1994
    Schlagwörter: aircraft control , Fuselage

    Design, Development and Testing of Airplanes for Mars Exploration

    D. W. Hall | NTIS | 2004
    Schlagwörter: Aircraft , Wing-fuselage stores

    Effect of impedance control of the response of aircraft digital subsystems to HIRF (high-incidence RF field)

    Slattery, K.P. / Fuller, G. | Tema Archiv | 1990
    Schlagwörter: AIRCRAFT INSTRUMENTATION , AIRCRAFT DIGITAL SUBSYSTEMS , FUSELAGE , AIRCRAFT CABLES

    Non-Linear Model for the Longitudinal Dynamics of a Hypersonic Air- breathing Vehicle

    M. A. Bolender / D. B. Doman | NTIS | 2006
    Schlagwörter: Aircraft , Hypersonic aircraft , Fuselage bending mode

    Three-dimensional Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow

    R. E. Bartels / J. J. McNamara / P. P. Friedmann et al. | NTIS | 2005
    Schlagwörter: Aircraft , Fuselage

    Exploratory Tests on a Forward-Mounted Overwing Engine Installation

    D. J. Kettle / A. G. Kurn / J. A. Bagley | NTIS | 1972
    Schlagwörter: Transport aircraft , Wing-fuselage stores

    Wing Design

    Sadraey, Mohammad H. | Wiley | 2012
    Schlagwörter: low‐ and high‐speed aircraft sweep angles , wing vertical location, relative to fuselage center line , wing incidence (iw), angle between fuselage center line and wing chord

    The development of a microcomputer CAD/CAM and decision support system for the manufacture of aerospace vehicles

    Scott, C.T. / Daily, M. | Tema Archiv | 1988
    Schlagwörter: AIRCRAFT DESIGN , FUSELAGE DESIGN PARAMETERS , AIRCRAFT COMPONENTS , COMPUTER-GENERATED AIRCRAFT , MINIATURE AIRCRAFT

    Airfoil Modification Effects on Subsonic and Transonic Pressure Distributions and Performance for the EA-6B Airplane

    D. O. Allison / W. G. Sewall | NTIS | 1995
    Schlagwörter: Aircraft models , Wing-fuselage stores

    RF Interoperability

    Macnamara, Thereza M. | Wiley | 2010
    Schlagwörter: Coupling between Systems for Antennas on Opposite Surfaces of the Fuselage , Coupling between Systems on an Aircraft

    Loads and Stability Analysis of an Unmanned Tilt Rotor

    M. W. Floros / J. Shen / M. K. Lee et al. | NTIS | 2006
    Schlagwörter: Aircraft , Tilt rotor aircraft , Fuselage roll inertia

    Hinfinity design of future flight control systems

    Colgren, R. | Tema Archiv | 1990
    Schlagwörter: AIRCRAFT CONTROL , FUSELAGE BENDING MODES

    Aerodynamic Design

    Seddon, John / Newman, Simon | Wiley | 2011
    Schlagwörter: design of rotor blade sections ‐ following lead by fixed‐wing aircraft , parasite drag ‐ helicopter parts, fuselage, rotor head, tail rotor and tail surfaces

    Trim, Stability and Control

    Seddon, John / Newman, Simon | Wiley | 2011
    Schlagwörter: balance of moments, aircraft centre of gravity (CG) ‐ attitude, adopted by airframe , flight principle, of any aircraft ‐ aerodynamic, gravitational forces and moments, in balance , fuselage attitude in forward flight ‐ forward CG, aft CG, forward CG with direct head moment

    Rotor Mechanisms for Forward Flight

    Seddon, John / Newman, Simon | Wiley | 2011
    Schlagwörter: Kaman aircraft, and slightly different system ‐ blade pitch, trailing edge servo flap control , stability variation ‐ fuselage and lag damping influence