Publication detail

Aerodynamic Design and Optimization of Single Slotted Flap

HRNČÍŘ, Z.

Original Title

Aerodynamic Design and Optimization of Single Slotted Flap

Type

journal article - other

Language

English

Original Abstract

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.

Key words in English

optimization CFD aerodynamic

Authors

HRNČÍŘ, Z.

RIV year

2003

Released

1. 1. 2003

Location

Vilnius Litva

ISBN

1648-7788

Periodical

AVIATION

Year of study

7

Number

3

State

Republic of Lithuania

Pages from

45

Pages to

48

Pages count

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"
}