Publication detail

Aerodynamic Design and Optimization of Single Slotted Flap

HRNČÍŘ, Z.

English title

Aerodynamic Design and Optimization of Single Slotted Flap

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

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.

Released

2003-01-01

Location

Vilnius Litva

ISSN

1648-7788

Book

Aviation

Journal

Aviation

Volume

7

Number

3

Pages from–to

45–

Pages count

4

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"
}