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Thursday, April 23, 2020 | History

3 edition of A zonal method for modeling powered-lift aircraft flow fields found in the catalog.

A zonal method for modeling powered-lift aircraft flow fields

Roberts, D. W.

A zonal method for modeling powered-lift aircraft flow fields

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  • 14 Currently reading

Published by National Aeronautics and Space Administration, Ames Research Center, For sale by the National Technical Information Service in Moffett Field, Calif, [Springfield, Va .
Written in English

    Subjects:
  • Aerodynamics.

  • Edition Notes

    Other titlesZonal method for modeling powered lift aircraft flow fields.
    StatementD.W. Roberts.
    SeriesNASA contractor report -- 177521., NASA contractor report -- NASA CR-177521.
    ContributionsAmes Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15289716M


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A zonal method for modeling powered-lift aircraft flow fields by Roberts, D. W. Download PDF EPUB FB2

Get this from a library. A zonal method for modeling powered-lift aircraft flow fields. [D W Roberts; Ames Research Center.]. Drag prediction method of powered-on civil aircraft based on thrust drag bookkeeping Article (PDF Available) in Chinese Journal of Aeronautics 24 June with Reads How we measure 'reads'.

The present conference discusses the comparative aerodynamic behavior of half-span and full-span delta wings, TRANAIR applications to engine/airframe integration, a zonal approach to V/STOL vehicle aerodynamics, an aerodynamic analysis of segmented aircraft configurations in high-speed flight, unstructured grid generation and FEM flow solvers, surface grid generation for flowfields using B.

Close Drawer Menu Close Drawer Menu Menu. Home; Journals. AIAA Journal; Journal of Aerospace Information Systems; Journal of Air Transportation; Journal of Aircraft; Journal of. A key enabler for the efficient design of powered lift systems for future STOL (Short Take-Off and Landing) aircraft is the ability to perform accurate CFD (Computational Fluid Dynamics.

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Topics of interest in the design, flow modeling and visualization, and turbulence and flow separation effects for low Reynolds number (Re) airfoils are discussed. Design methods are presented for Re f, including a viscous-inviscid coupling method and by.

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The work aims to develop a class of modular semi-empirical dynamic. Computational Fluid Dynamics “This page left intentionally blank.” 5 Invited Lectures and 3 Keynote Lectures were delivered by renowned researchers in the areas of innovative modeling of flow physics, innovative algorithm development for flow simulation, optimization and control, and advanced multidisciplinary applications.

HIGH-LIFT AERODYNAMICS. method and ideas in this paper, mainly because of their great convenience. Figure 15 summarizes the prediction accuracy of the Cebeci-Smith method. The data consist of the results from Ref. 23 together with other, unpublished studies.

A Zonal Method for Modeling Flow Fields of Powered-Lift Aircraft Abstract: Advanced short takeoff/vertical landing aircraft are designed to use exhaust jets directly to increase lift. Being able to numerically model the flow fields involved in these designs would greatly improve the design process.

Absorbent Testing and Mathematical Modeling of a Solid Amine Regenerative CO~2 and H~2O Removal System. Recent Applications of the FNS Zonal Method to Complex Flow Problems. Fujii, K. / Tamura, Y. | Gedruckte Ausgabe A Simulator Study of a Flight Reference Display for Powered-Lift STOL Aircraft.

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