Synonyms were used for: Aircraft Design
Search without synonyms: title: Aircraft Aerodynamic Design

41–60 of 335 hits
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    Analysis of the Aerodynamic Design of the P-47B Airplane

    M J Brevoort / George W Stickle | NTRS | 1942
    The subject airplane has several features which have an influence on its aerodynamic and cooling performance. The purpose of this ...
    Keywords: Aircraft Design, Testing And Performance

    Disciplinary Sub-Processes to Assess Low-Speed Performance and Noise Characteristics within an Aircraft Design Environment

    Fröhler, B. / Hesse, C. / Atanasov, G. et al. | DataCite | 2021
    The overall aircraft assessment is based on a wide range of disciplinary methodologies. In addition, a consistent aircraft design must be ...
    Keywords: Conceptual aircraft design , multidisciplinary design and analysis , Aircraft noise prediction

    Procedure for automating aircraft wing structural design

    Giles, G. L. | NTRS | 1971
    Aircraft wings automated preliminary structural design and weight determination procedures based on external shape, aerodynamic loads and ...

    Influence of a Detailed Mass Estimation for a Wing with known Flight Shape in Conceptual Overall Aircraft Design

    Effing, T. / Stephan, R. / Stumpf, E. | DataCite | 2023
    (VC) application exhibits—from an overall aircraft design perspective—minor differences in the flight shape and, thus, in the aerodynamic ...
    Keywords: Conceptual aircraft design , short-medium range aircraft

    Aerodynamic characteristics of supersonic fighter airplane configurations based on Soviet design concepts

    Spearman, M. L. / Fournier, R. H. / Lamb, M. | NTRS | 1977
    , which are based on Soviet design concepts, include fixed-wing aircraft having delta wings, swept wings, and trapezoidal wings, and a variable ...
    Keywords: Aircraft Design, Testing And Performance

    Variable Camber Continuous Aerodynamic Control Surfaces and Methods for Active Wing Shaping Control

    Nguyen, Nhan T. | NTRS | 2016
    An aerodynamic control apparatus for an air vehicle improves various aerodynamic performance metrics by employing multiple spanwise flap ...
    Keywords: Aircraft Design, Testing And Performance

    AERODYNAMIC FACTORS TO BE CONSIDERED IN THE DESIGN OF TILT-WING V/STOL AIRPLANES

    Kirby, R. H. / Mc Kinney, M. O. / Newsom, W. A. | NTRS | 1963
    Aerodynamic considerations in the design of tilt-wing v/stol aircraft ...
    Keywords: STOL AIRCRAFT , TILT-WING AIRCRAFT , VTOL AIRCRAFT , AIRCRAFT DESIGN

    Learn-To-Fly Project Overview: In-Flight and Wind Tunnel Global Nonlinear Aerodynamic Modeling

    Jay Brandon | NTRS | 2014
    Keywords: Aircraft Design, Testing and Performance

    Aerostructural Optimization of a Flexible-Winged Aircraft Using OpenVSP

    Tim Brooks | NTRS
    MBSAE project connecting aircraft geometry tool, OpenVSP, to opensourace aerodynamic, OpenAeroStruct, and structural, TACS, solvers using ...
    Keywords: Aircraft Design, Testing And Performance

    Conceptual Design and Comparative Study of Strut-Braced Wing and Twin-Fuselage Aircraft Configurations with Ultra-High Aspect Ratio Wings

    Ma, Yiyuan / Karpuk, Stanislav / Elham, Ali | DataCite | 2021
    ratio wings (UHARW) configuration is one key enabling strategy for improving aircraft aerodynamic efficiency and reducing fuel consumption and ...

    Determining Aircraft Moments of Inertia from Flight Test Data

    Eugene A Morelli | NTRS | 2021
    expansions in the aircraft states and controls. Aerodynamic parameters were estimated simultaneously with inertia parameters using equation-error ...
    Keywords: Aircraft Design, Testing And Performance

    Determining Aircraft Moments of Inertia from Flight Test Data

    Gene Morelli | NTRS
    Flight test maneuver design and dynamic modeling techniques were developed for determining aircraft moments of inertia from flight test ...
    Keywords: Aircraft Design, Testing And Performance , Aircraft Moments of Inertia , Aircraft Stability And Control

    Aerodynamic preliminary analysis

    Bonner, E. / Clever, W. / Divan, P. et al. | NTRS | 1981
    Computerization of aerodynamic theory has progressed to state where analysis of complete aircraft configurations can be performed in single ...

    Validation of a Mid-Fidelity Approach for Aircraft Stability and Control Characterization

    Benjamin M. Simmons / Steven C. Geuther / Vivek Ahuja | NTRS
    Keywords: aerodynamic modeling , Aircraft Stability and Control , Aircraft Design, Testing and Performance , aerodynamic prediction methods

    Modeling and parameter uncertainties for aircraft flight control system design

    Rickard, W. W. | NTRS | 1978
    values of plant uncertainties for some recent aircraft design and development programs. Histories of pertinent aerodynamic, inertial, and ...
    Keywords: Aircraft Stability And Control

    X-34 Vehicle Aerodynamic Characteristics

    Brauckmann, Gregory J. | NTRS | 1998
    from an L-1011 carrier aircraft at approximately Mach 0.7 and 38,000 feet altitude, where an onboard engine will accelerate the vehicle to ...
    Keywords: Spacecraft Design, Testing And Performance

    Aerodynamic Heating and Fatigue

    Kroll, Wilhelmina D. | NTRS | 1959
    the design has been established. A survey of the literature shows what phases of elevated-temperature fatigue have been investigated. Other ...

    Integrated aerodynamic load/dynamic optimization of helicopter rotor blades

    Chattopadhyay, Aditi / Walsh, Joanne L. / Riley, Michael F. | NTRS | 1991
    Keywords: Aircraft Design, Testing And Performance

    Inlet Trade Study for a Low-Boom Aircraft Demonstrator

    Heath, Christopher M. / Slater, John W. / Rallabhandi, Sriram K. | NTRS | 2016
    Propulsion integration for low-boom supersonic aircraft requires careful inlet selection, placement, and tailoring to achieve acceptable ...
    Keywords: Aircraft Design, Testing And Performance

    Sizing Studies of Light Aircraft with Serial Hybrid Propulsion Systems

    Ludowicy, J. / Rings, R. / Finger, D.F. et al. | DataCite | 2018
    conventionally powered aircraft with similar specifications, by the means of initial sizing results. Studies on battery specific energy and aerodynamic ...
    Keywords: Aircraft Preliminary Sizing