All

What are you looking for?

All
Projects
Results
Organizations

Quick search

  • Projects supported by TA ČR
  • Excellent projects
  • Projects with the highest public support
  • Current projects

Smart search

  • That is how I find a specific +word
  • That is how I leave the -word out of the results
  • “That is how I can find the whole phrase”

Note on the Physical Basis of the Kutta Condition in Unsteady Two-Dimensional Panel Methods

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216208%3A11320%2F15%3A10320083" target="_blank" >RIV/00216208:11320/15:10320083 - isvavai.cz</a>

  • Result on the web

    <a href="http://dx.doi.org/10.1155/2015/708541" target="_blank" >http://dx.doi.org/10.1155/2015/708541</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1155/2015/708541" target="_blank" >10.1155/2015/708541</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Note on the Physical Basis of the Kutta Condition in Unsteady Two-Dimensional Panel Methods

  • Original language description

    Force generation in avian and aquatic species is of considerable interest for possible engineering applications. The aim of this work is to highlight the theoretical and physical foundations of a new formulation of the unsteady Kutta condition, which postulates a finite pressure difference at the trailing edge of the foil. The condition, necessary to obtain a unique solution and derived from the unsteady Bernoulli equation, implies that the energy supplied for the wing motion generates trailing-edge vortices and their overall effect, which depends on themotion initial parameters, is a jet of fluid that propels the wing. The postulated pressure difference (the value of which should be experimentally obtained) models the trailing-edge velocity differencethat generates the thrust-producing jet. Although the average thrust values computed by the proposed method are comparable to those calculated by assuming null pressure difference at the trailing edge, the latter (commonly used) approach

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

  • CEP classification

    BK - Liquid mechanics

  • OECD FORD branch

Result continuities

  • Project

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2015

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Name of the periodical

    Mathematical Problems in Engineering

  • ISSN

    1024-123X

  • e-ISSN

  • Volume of the periodical

    neuveden

  • Issue of the periodical within the volume

    November 2015

  • Country of publishing house

    US - UNITED STATES

  • Number of pages

    8

  • Pages from-to

    1-8

  • UT code for WoS article

    000360235200001

  • EID of the result in the Scopus database

    2-s2.0-84940116827