Synonyme wurden verwendet für: Aircraft
Suche ohne Synonyme: title: AIAA Journal of Aircraft

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    Small Airplane Considerations for the Guidelines for Development of Civil Aircraft and Systems

    Voros, Robert E. | SAE Technical Papers | 2013
    On September 30, 2011, certification authorities released Advisory Circular 20-174[1], Development of Civil Aircraft and Systems, which ...
    Verlag: Society of Automotive Engineers , SAE International
    Schlagwörter: Aircraft

    Vortex interactions and decay in aircraft wakes

    Bilanin, A. J. / Teske, M. E. / Williamson, G. G. | NTRS | 1977
    The dynamic interactions of aircraft wake vortices are investigated using both inviscid and viscous models. The phenomenon of vortex ...

    Second derivatives of the flutter velocity and the optimization of aircraft structures.

    Rudisill, C. S. / Bhatia, K. G. | NTRS | 1972
    partial derivatives of the flutter velocity of an aircraft structure with respect to the structural parameters are derived. These partial ...

    Special section on Second Sonic Boom Prediction Workshop

    AIAA Sonic Boom Prediction Workshop / American Institute of Aeronautics and Astronautics | TIBKAT | 2019
    Verlag: American Institute of Aeronautics and Astronautics , Reston, VA

    Effect of High-Fidelity Ice Accretion Simulations on the Performance of a Full-Scale Airfoil Model

    Broeren, Andy P. / Bragg, Michael B. / Addy, Harold E., Jr. et al. | NTRS | 2010
    The simulation of ice accretion on a wing or other surface is often required for aerodynamic evaluation, particularly at small scale or low ...

    Methods for Prediction of High-Speed Reacting Flows in Aerospace Propulsion

    Drummond, J. Philip | NTRS | 2014
    Research to develop high-speed airbreathing aerospace propulsion systems was underway in the late 1950s. A major part of the effort ...
    Schlagwörter: Aircraft Design, Testing And Performance

    Nonlinear Aerodynamics of Bodies in Coning Motion

    Schiff, Lewis B. | NTRS | 1972
    permits accurate computation of the aerodynamic moment due to one of the four motions characterizing an arbitrary nonplanar motion. Results of ...
    Verlag: American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Design, Testing And Performance

    Suspension-line wave motion during the lines-first parachute unfurling process

    Poole, L. R. / Whitesides, J. L. | NTRS | 1974
    distinct phases: a suspension-line unfurling phase, during which a massless-spring model of the suspension-line elasticity may be employed; and a ...
    Schlagwörter: Aircraft

    Equivalent Plate Structural Modeling for Wing Shape Optimization Including Transverse Shear

    Livne, Eli | NTRS | 1994
    A new technique for structural modeling of airplane wings is presented taking transverse shear effects into account. The kinematic ...
    Verlag: American Institute of Aeronautics and Astronautics, Inc.
    Schlagwörter: Aircraft Design, Testing And Performance

    Study of Ice Accretion Physics to Improve the Ice Accretion on Airfoils

    M. B. Bragg | NTIS | 2001
    the icing wind tunnel turbulence work was published in the archival AIAA Journal of Aircraft. A brief summary of the findings is given. Please ...

    A similarity analysis of the droplet trajectory equation

    Bragg, M. B. | NTRS | 1982
    A procedure is established to reduce the number of similarity parameters in the trajectory equation for particles in a moving fluid. This ...

    A Study of Ice Accretion Physics to Improve the Ice Accretion on Airfoils

    Bragg, Michael B. | NTRS | 2001
    the icing wind tunnel turbulence work was published in the archival AIAA Journal of Aircraft. A brief summary of the findings is given. Please ...

    Discrete-Roughness-Element-Enhanced Swept-Wing Natural Laminar Flow at High Reynolds Numbers

    Malik, Mujeeb / Liao, Wei / Li, Fei et al. | NTRS | 2015
    transport aircraft. Computations performed for the boundary layer on a natural-laminar-flow airfoil with a leading-edge sweep angle of 34.6 deg ...

    Aero-Structural Optimization of HSCT Configurations in Transonic and Supersonic Flow

    J. J. Alonso | NTIS | 1999
    conference and journal publications. The following sections summarize the technical accomplishments obtained during the last year. Details of these ...
    Schlagwörter: Aircraft , Aircraft configurations

    Adjoint-Based Methodology for Time-Dependent Optimal Control (AMTOC)

    Yamaleev, Nail / Diskin, boris / Nishikawa, Hiroaki | NTRS | 2012
    aerodynamic systems, such as fighter jet, subsonic aircraft, rotorcraft, high-lift, wind-turbine, and flapping-wing configurations. In the course of ...

    Compliance with High-Intensity Radiated Fields Regulations - Emitter's Perspective

    Statman, Joseph I. / Nguyen, Lee / Jamnejad, Vahraz | SAE Technical Papers | 2012
    protection for aircraft electrical and electronic systems (Title 14, Code of Federal Regulations (14 CFR) §§ 23.1308, 25.1317, 27.1317, and 29.1317 ...
    Verlag: Society of Automotive Engineers , SAE International
    Schlagwörter: Aircraft

    Nonlinear filtering for random signals in statistically unknown noise.

    Loo, J. T. | NTRS | 1972
    Natural and effective formulation of the filtering problem involved in satellite orbit determination, aircraft navigation, and missile ...

    Structural synthesis - Its genesis and development

    Schmit, L. A. | NTRS | 1981
    plate, a stiffened cylindrical shell, aircraft fuselage window panels, the structural efficiency of graphite-epoxy hat-stiffened panels, and an ...

    Instrumental variables algorithm for modal parameter identification in flutter testing

    Johnson, W. / Gupta, N. K. | NTRS | 1978
    The paper is concerned with the task of estimating modal parameters from system response measurement in aircraft flutter testing. A ...

    Trends and pacing items in computational aerodynamics

    Chapman, D. R. | NTRS | 1981
    applications. From a survey of AIAA Journal papers published during the past two decades, the growth trends and the progressively increasing emphasis ...