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

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    Challenges and Progress in Aerodynamic Design of Hybrid Wingbody Aircraft with Embedded Engines

    Liou, Meng-Sing / Kim, Hyoungjin / Liou, May-Fun | NTRS | 2016
    We summarize the contributions to high-fidelity capabilities for analysis and design of hybrid wingbody (HWB) configurations considered by ...
    Keywords: design optimization , aerodynamic performance , Aircraft Design, Testing And Performance , Aircraft Propulsion And Power

    Aerodynamic analysis of hypersonic waverider aircraft

    Sandlin, Doral R. / Pessin, David N. | NTRS | 1993
    they can be used to generate and analyze waverider aircraft at on-design and off-design conditions. To generate waverider configurations and ...

    Aerodynamic Performance Studies for Supersonic Cruise Aircraft

    Mascitti, V. R. | NTRS | 1976
    Technical progress made in each of the disciplinary research areas affecting the design of supersonic cruise aircraft is discussed. The ...

    Identification of aerodynamic models for maneuvering aircraft

    Chin, Suei / Lan, C. Edward | NTRS | 1990
    mathematical modeling to describe the steady and unsteady aerodynamics for the aircraft equations of motion. Aerodynamic forces and moments acting on a ...

    Exploration of Design Drivers for the RVLT Lift+Cruise Reference Aircraft

    Jason R. Welstead | NTRS | 2023
    were performed using the NASA Design and Analysis of Rotorcraft tool and a Rapid Sizing Tool for electric vertical takeoff and landing aircraft ...
    Keywords: Aircraft Propulsion and Power

    Aerodynamic Design and Computational Analysis of a Spacecraft Cabin Ventilation Fan

    Tweedt, Daniel L. | NTRS | 2010
    methodologies similar to those employed by the aircraft engine industry, most notably computational fluid dynamics (CFD) codes, the aerodynamic design ...

    Deployable aerodynamic decelaration systems - Space vehicle design criteria

    NTRS | 1971
    Criteria and recommended practices for design, selection, analysis, and testing of deployable aerodynamic deceleration systems ...
    Keywords: Aircraft

    Multidisciplinary Design Optimization and Cruise Mach Number Study of Truss-Braced Wing Aircraft

    Kapania, Rakesh K. / Schetz, Joseph A. / Mallik, Wrik et al. | NTRS | 2018
    The Subsonic Ultra Green Aircraft Research (SUGAR) Phase III was led by Dr. Rakesh K. Kapania and Dr. Joseph A. Schetz at the ...
    Keywords: Aircraft Design, Testing And Performance

    Study of aerodynamic technology for VSTOL fighter/attack aircraft, volume 1

    Lummus, J. R. | NTRS | 1978
    An assessment was made of the aerodynamic uncertainties associated with the design of a cold-deck-environment Navy VSTOL fighter/attack ...

    Study of aerodynamic technology for VSTOL fighter/attack aircraft, phase 1

    Driggers, H. H. | NTRS | 1978
    A conceptual design study was performed of a vertical attitude takeoff and landing (VATOL) fighter/attack aircraft. The configuration has a ...

    Formulation of aerodynamic prediction techniques for hypersonic configuration design

    NTRS | 1979
    An investigation of approximate theoretical techniques for predicting aerodynamic characteristics and surface pressures for relatively ...
    Keywords: Aircraft Design, Testing And Performance

    Aircraft empennage structural detail design

    Lesnewski, David / Snow, Russ M. / Combs, Lisa M. et al. | NTRS | 1993
    durable lightweight structure that will transfer the aerodynamic forces produced by the tail surfaces through the most efficient load path to the ...
    Keywords: Aircraft Design, Testing And Performance

    Flight testing a V/STOL aircraft to identify a full-envelope aerodynamic model

    Mcnally, B. David / Bach, Ralph E., Jr. | NTRS | 1988
    Flight-test techniques are being used to generate a data base for identification of a full-envelope aerodynamic model of a V/STOL fighter ...
    Keywords: Aircraft Design, Testing And Performance

    The aerodynamic design of the oblique flying wing supersonic transport

    Vandervelden, Alexander J. M. / Kroo, Ilan | NTRS | 1990
    The aerodynamic design of a supersonic oblique flying wing is strongly influenced by the requirement that passengers must be accommodated ...
    Keywords: Aircraft Design, Testing And Performance

    Aerodynamic Parameters of High Performance Aircraft Estimated from Wind Tunnel and Flight Test Data

    Klein, Vladislav / Murphy, Patrick C. | NTRS | 1998
    A concept of system identification applied to high performance aircraft is introduced followed by a discussion on the identification ...
    Keywords: Aircraft Design, Testing And Performance

    Study of aerodynamic technology for VSTOL fighter/attack aircraft: Vertical attitude concept

    Gerhardt, H. A. / Chen, W. S. | NTRS | 1978
    The aerodynamic technology for a vertical attitude VSTOL (VATOL) supersonic fighter/attack aircraft was studied. The selected configuration ...

    Aerodynamic configuration development of the highly maneuverable aircraft technology remotely piloted research vehicle

    Gingrich, P. B. / Child, R. D. / Panageas, G. N. | NTRS | 1977
    The aerodynamic development of the highly maneuverable aircraft technology remotely piloted research vehicle (HiMAT/RPRV) from the ...

    Euler Technology Assessment for Preliminary Aircraft Design-Unstructured/Structured Grid NASTD Application for Aerodynamic Analysis of an Advanced Fighter/Tailless Configuration

    Michal, Todd R. | NTRS | 1998
    This study supports the NASA Langley sponsored project aimed at determining the viability of using Euler technology for preliminary design ...

    Study of aerodynamic technology for single-cruise engine V/STOL fighter/attack aircraft

    Driggers, H. H. / Powers, S. A. / Roush, R. T. | NTRS | 1982
    A conceptual design analysis is performed on a single engine V/STOL supersonic fighter/attack concept powered by a series flow tandem fan ...