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Optimization of Aerodynamic Drag of Three General Wing Geometries and Wing with Bell-Shaped Lift Distribution Having a Given Lift and a Given Bending Moment

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F20%3AN0000007" target="_blank" >RIV/00010669:_____/20:N0000007 - isvavai.cz</a>

  • Result on the web

    <a href="https://controls.papercept.net/conferences/scripts/rtf/IACAS20_ContentListWeb_1.html" target="_blank" >https://controls.papercept.net/conferences/scripts/rtf/IACAS20_ContentListWeb_1.html</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1051/matecconf/201930402005" target="_blank" >10.1051/matecconf/201930402005</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Optimization of Aerodynamic Drag of Three General Wing Geometries and Wing with Bell-Shaped Lift Distribution Having a Given Lift and a Given Bending Moment

  • Original language description

    In this article different wings are optimized by low and verified by high-fidelity methods to compare their aerodynamic characteristics. The unusual properties of the wing with the bell-shaped lift distribution is a reason why several general geometrical variants of the wings are compared. Three general wings are assumed and their geometry is defined as rectangular, trapezoidal and elliptical. Airspeed, total lift force and shape of the airfoil are defined, and bending moment is assumed as a surrogate model for wing weight. Minimizing of aerodynamic drag is a goal of optimization.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

    <a href="/en/project/LTARF18040" target="_blank" >LTARF18040: Advanced Composite Structure for Perspective Regional Aircraft</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2020

  • Confidentiality

    C - Předmět řešení projektu podléhá obchodnímu tajemství (§ 504 Občanského zákoníku), ale název projektu, cíle projektu a u ukončeného nebo zastaveného projektu zhodnocení výsledku řešení projektu (údaje P03, P04, P15, P19, P29, PN8) dodané do CEP, jsou upraveny tak, aby byly zveřejnitelné.

Data specific for result type

  • Article name in the collection

    AEROSPACE SCIENCES. ISRAEL ANNUAL CONFERENCE. 60TH 2020

  • ISBN

    9781713813552

  • ISSN

  • e-ISSN

  • Number of pages

    11

  • Pages from-to

    nestrankovano

  • Publisher name

    Curran Associates, Inc., 57 Morehouse Lane, Red Hook, NY 12571

  • Place of publication

    Technion Israel Institute of Technology

  • Event location

    Tel Avivi, Israel

  • Event date

    Mar 4, 2019

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article