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

81–100 of 335 hits
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    Evaluation of Response Surface Experiment Designs for Distributed Propulsion Aircraft Aero-Propulsive Modeling

    Benjamin M Simmons | NTRS
    Keywords: Aircraft Stability and Control , design of experiments , aerodynamic modeling , Aircraft Design, Testing and Performance

    Recent Dynamic Measurements and Considerations for Aerodynamic Modeling of Fighter Airplane Configurations

    Brandon, Jay M. / Foster, John V. | NTRS | 1998
    Keywords: Aircraft Design, Testing And Performance

    Longitudinal aerodynamic characteristics of light, twin-engine, propeller-driven airplanes

    Wolowicz, C. H. / Yancey, R. B. | NTRS | 1972
    Representative state-of-the-art analytical procedures and design data for predicting the longitudinal static and dynamic stability and ...
    Keywords: Aircraft

    Blade and Trajectory Optimization of a Propeller-Driven Electric Aircraft with Acoustic Constraints

    Daniel Ingraham / Robert Falck / Justin Gray | NTRS
    to meet this challenge. As a first step toward providing these tools, a propeller design toolchain that includes aerodynamic performance ...

    Design of P-3 Nadir Port

    Chance, Monica | NTRS | 2019
    potential approaches. In addition, design of a new interface to replace the existing plug, on an aircraft designed in the 1960's by Lockheed for the ...
    Keywords: Aircraft Design, Testing And Performance

    Two-Stage Axial Compressor Rig Designed To Develop and Validate Advanced Aerodynamic Technologies

    Larosiliere, Louis M. | NTRS | 2003
    aerodynamic design capability is required not only to maximize the specific thrust of next-generation engines without sacrificing fuel consumption ...
    Keywords: Aircraft Propulsion And Power

    Aerodynamic characteristics of a large-scale, twin tilt-nacelle V/STOL model

    Falarski, M. D. / Dudley, M. R. / Buchmann, W. et al. | NTRS | 1982
    A subsonic tilt-nacelle V/STOL aircraft configuration is described which is powered by two turbofan engines, mounted on a single carry ...
    Keywords: Aircraft Design, Testing And Performance

    Advanced supersonic cruise aircraft technology

    Baber, H. T., Jr. / Driver, C. | NTRS | 1977
    emphasis on aerodynamic characteristics, noise and chemical emission, and mission analysis. A recently developed aircraft sizing and performance ...
    Keywords: Aircraft Design, Testing And Performance

    Aerodynamic surface distension system for high angle of attack forebody vortex control

    Zell, Peter T. | NTRS | 1994
    two inflatable membranes are located on the forebody portion of an aircraft on opposite sides thereof. The members form control surfaces for ...
    Keywords: Aircraft Design, Testing And Performance

    Design and Evaluation of a Turbojet Exhaust Simulator, Utilizing a Solid-Propellant Rocket Motor, for use in Free-Flight Aerodynamic Research Models

    deMoraes, Carlos A. / Hagginbothom, William K., Jr. / Falanga, Ralph A. | NTRS | 1954
    analysis necessary to the design is presented along with tests from which the designs are evaluated. Simulation was found to be best if the exhaust ...
    Keywords: Aircraft Propulsion And Power

    Aerodynamic Characteristics of a 45 Degree Swept-wing Fighter-Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53

    Oehman, Waldo I / Turner, Kenneth L | NTRS | 1958
    An investigation was performed in the Langley Unitary Plan wind tunnel to determine the aerodynamic characteristics of a model of a 450 ...
    Keywords: Aircraft Design, Testing And Performance

    Flutter testing of modern aircraft

    Johnson, Jeff | NTRS | 1989
    Structural dynamicists avoid aircraft structural flutter through the use of flutter analyses, wind tunnel tests, ground-vibration tests ...
    Keywords: Aircraft Design, Testing And Performance

    Fundamental aerodynamic characteristics of delta wings with leading-edge vortex flows

    Wood, R. M. / Miller, D. S. | NTRS | 1985
    number and to increase nonlinearly, with an increasing slope, with increasing angle of attack. These charts are then used to define a wing-design ...

    The NASA Aircraft Energy Efficiency program

    Klineberg, J. M. | NTRS | 1979
    propulsive, aerodynamic and structural efficiency for future transport aircraft. Attention is given to engine component improvement, an energy ...
    Keywords: Aircraft Design, Testing And Performance

    Free wing assembly for an aircraft

    Wolowicz, C. H. | NTRS | 1978
    A free wing is attached to a fuselage of an aircraft in a manner such that the wing is free to pivot about a spanwise axis forward of its ...
    Keywords: Aircraft Design, Testing And Performance

    Aero-Propulsive Modeling for eVTOL Aircraft Using Wind Tunnel Testing with Multisine Inputs

    Benjamin M. Simmons / Eugene A. Morelli / Ronald C. Busan et al. | NTRS
    Keywords: design of experiments , aerodynamic modeling , Aircraft Stability And Control

    Aerodynamic Characteristics of a Number of Modified NACA Four-Digit-Series Airfoil Sections

    Loftin, Laurence K., Jr. / Cohen, Kenneth G. | NTRS | 1947
    Keywords: Aircraft Design, Testing And Performance

    Lateral-directional aerodynamic characteristics of light, twin-engine, propeller driven airplanes

    Wolowicz, C. H. / Yancey, R. B. | NTRS | 1972
    Analytical procedures and design data for predicting the lateral-directional static and dynamic stability and control characteristics of ...
    Keywords: Aircraft

    Computational and experimental studies of light twin aerodynamic interference

    Thomson, W. G. / Wentz, W. H., Jr. / Ostowari, C. | NTRS | 1982
    The results of an analytical and experimental study of aerodynamic interference effects for a light twin aircraft are presented. Both the ...

    Current Methods Modeling and Simulating Icing Effects on Aircraft Performance, Stability, Control

    Ratvasky, Thomas P. / Barnhart, Billy P. / Lee, Sam | NTRS | 2010
    Icing alters the shape and surface characteristics of aircraft components, which results in altered aerodynamic forces and moments caused ...
    Keywords: Aircraft Design, Testing And Performance