Detail publikace

Aerodynamic Design and Optimization of Single Slotted Flap

HRNČÍŘ, Z.

Originální název

Aerodynamic Design and Optimization of Single Slotted Flap

Typ

článek v časopise - ostatní, Jost

Jazyk

angličtina

Originální abstrakt

The method for aerodynamic design and optimization of single slotted flap is presented. As a tool for preliminary design of flap shape a panel method is used. The flap position in the landing configuration is optimized. The Nelder-Mead simplex method is used as optimization algorithm. The aerodynamic performance is predicted using commercial CFD software Fluent 6. The design/optimization approach is first validated by calculation of NACA 23012 airfoil with single slotted flap and by comparing with experimental investigation. Results show the appropriateness of the approach for design and optimization of single slotted flap.

Klíčová slova v angličtině

optimization CFD aerodynamic

Autoři

HRNČÍŘ, Z.

Rok RIV

2003

Vydáno

1. 1. 2003

Místo

Vilnius Litva

ISSN

1648-7788

Periodikum

AVIATION

Ročník

7

Číslo

3

Stát

Litevská republika

Strany od

45

Strany do

48

Strany počet

4

URL

Letecký Ústav

BibTex

@article{BUT41146,
  author="Zbyněk {Hrnčíř}",
  title="Aerodynamic Design and Optimization of Single Slotted Flap",
  journal="AVIATION",
  year="2003",
  volume="7",
  number="3",
  pages="4",
  issn="1648-7788",
  url="Letecký Ústav"
}