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

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    Aerodynamic Design of Integrated Propulsion-Airframe Configuration of the Hybrid Wing-Body Aircraft

    Liou, May-Fun / Kim, Hyoungjin / Lee, B. J. et al. | NTRS | 2017
    Hybrid Wing Body (HWB) aircraft is characterized by a flattened and airfoil-shaped body, which produces a substantial portion of the total ...
    Keywords: Aircraft Design, Testing And Performance

    Aerodynamic Decelerator System Design

    Machin, Ricardo | NTRS | 2010
    Keywords: Aircraft Design, Testing And Performance

    Enhancement of an Aircraft Design Environment for the Design of Fighter Aircraft

    Hasenau, M.A.C. / Varga, S.A. / Scholz, A.E. et al. | DataCite | 2021
    aircraft. New design challenges were, among others, the approximation of the aerodynamic and geometrical effects of supersonic flight and increased ...
    Keywords: fighter aircraft , aircraft design

    Investigation of Aerodynamic Matching Sensitivities for Conceptual Design

    Jesse Ray Quinlan / Zachary Dell Windous / Frank H Gern et al. | NTRS
    A methodology for aerodynamic matching was implemented in the Higher fidelity Conceptual Design and structural optimization (HCDstruct ...
    Keywords: Aircraft Design, Testing And Performance

    Approach for the Aerodynamic Optimization of the Twist Distribution of Arbitrary Wing Geometries on Conceptual Aircraft Design Level

    Effing, T. / Peter, F. / Stumpf, E. et al. | DataCite | 2021
    This paper presents an approach for consciously tailoring the lift distribution of a given wing geometry in early stages of aircraft design ...
    Keywords: Conceptual aircraft design

    Approach for the Aerodynamic Optimization of the Twist Distribution of Arbitrary Wing Geometries on Conceptual Aircraft Design Level

    Effing, Tim / Peter, F. / Stumpf, Eike et al. | DataCite | 2022
    Keywords: Conceptual aircraft design

    Aerodynamic Design and Wind Tunnel Test of a Laminar Wing with Split Flap for a Fuel Cell Powered Aircraft

    Free access
    Frey, J. / Sell, F. / Gillespy, R. et al. | DataCite | 2021
    This paper presents a wing design for the APUS i-2 concept hydrogen fuel cell aircraft that meets design requirements for hydrogen storage ...

    Preliminary Research Aerodynamic Design to Land on Mars

    Berger, David | NTRS | 2018
    Keywords: Aircraft Design, Testing And Performance

    Efficient Variable-Pitch Propeller Aerodynamic Model Development for Vectored-Thrust eVTOL Aircraft

    Benjamin M. Simmons | NTRS
    Keywords: design of experiments , aerodynamic modeling , Aircraft Stability And Control

    History and Status of the CDISC Aerodynamic Design Method

    Richard L. Campbell / Michelle N. Banchy / Brett R. Hiller | NTRS
    This paper will review the development and application of the CDISC aerodynamic design method that began in the early 1980s and continues ...
    Keywords: Aerodynamic design , Knowledge-based design

    Special Course on Engineering Methods in Aerodynamic Analysis and Design of Aircraft

    Advisory Group for Aerospace Research and Development | NTRS | 1992
    Lecture notes for the AGARD Fluid Dynamics Panel Special Course on 'Engineering Methods in Aerodynamic Analysis and Design of Aircraft ...
    Keywords: Aircraft Design, Testing And Performance , aircraft design , design analysis

    Modeling Programs Increase Aircraft Design Safety

    NTRS | 2012
    . Flutter occurs when aerodynamic forces acting on a wing cause it to vibrate. As the aircraft moves faster, certain conditions can cause that ...

    Aerodynamic Characteristics of Propeller-Driven VTOL Aircraft

    Kirby, Robert H. | NTRS | 1961
    Keywords: Aircraft Design, Testing And Performance

    Rotor blade aerodynamic design

    Walsh, Joanne L. / Noonan, Kevin W. | NTRS | 1989
    Aerodynamic performance aspects of rotor blade design are presented. Design considerations, aerodynamic constraints and design variables ...
    Keywords: Aircraft Design, Testing And Performance

    Transonic Cruise Slotted Wing Design for Commercial Transport Aircraft using CDISC

    Brett Hiller / Richard Campbell / Michelle Banchy | NTRS
    A knowledge-based aerodynamic design method, CDISC, has been extended to enable the computational design of transonic cruise slotted wings ...
    Keywords: Aerodynamic Design

    Preliminary overall aircraft design with hybrid laminar flow control

    Risse, Kristof | DataCite | 2016
    This thesis deals with preliminary overall aircraft design including hybrid laminar flow control (HLFC) on wings and tails. An integrated ...
    Keywords: Flugzeugentwurf ; Aircraft Design ; Wing Design ; Hybrid Laminar Flow Control ; HLFC

    High-Lift-System Design for a Low-Noise Medium-Range Aircraft

    Free access
    Schmidt, F.N. / Keller, D. / Iwanizki, M. et al. | DataCite | 2024
    The DLR project "Low noise medium-range aircraft" (SIAM) has set itself the goal of designing an aircraft with the boundary conditions of ...
    Keywords: Aerodynamic Design , Low-Noise Aircraft

    FlightStream® Technology Empowers NASA Engineers to Design Unconventional Aircraft

    Kimberly A Cannon / Bailey Grace Light | NTRS | 2020
    aerodynamic performance and feasibility of aircraft concepts, particularly those with no historical performance data. The company has since gained ...
    Keywords: Aircraft Design, Testing And Performance

    Aerodynamic and structural studies of joined-wing aircraft

    Kroo, Ilan / Smith, Stephen / Gallman, John | NTRS | 1991
    A method for rapidly evaluating the structural and aerodynamic characteristics of joined-wing aircraft was developed and used to study the ...
    Keywords: Aircraft Design, Testing And Performance

    Initial Weight Estimation of Twin Fuselage Configuration in Aircraft Conceptual Design

    Ma, Yiyuan / Yan, Jin / Elham, Ali | DataCite | 2021
    The Ultra High Aspect Ratio Wing (UHARW) concept can improve the aircraft 's aerodynamic efficiency and reduce fuel consumption. T he Twin ...
    Keywords: Twin fuselage configurati on, initial weight estimation, vortex lattice m ethod, composite materials, aircraft conceptual design