Publication detail

OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING

PEŠÁK, M. PÍŠTĚK, A.

Czech title

OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING

English title

OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING

Type

journal article - other

Language

cs

Original abstract

In modern aircraft structural design, the high accuracy calculation to obtain the highest efficiency of the structure is possible through the use of computer analysis. A system of computer programs to optimize and analyze skin-stringer panel for fuselage and lifting surfaces (wing and empennage structures) is being developed at the Institute of aerospace engineering, FME, BUT now. This paper deals with the optimum design of the reinforced panel which means Skin – stringer Panel. This form of construction is a logical development of the necessity of providing a continuous surface for an airplane, combined with the requirement that the weight of structure should be as small as possible.

Czech abstract

In modern aircraft structural design, the high accuracy calculation to obtain the highest efficiency of the structure is possible through the use of computer analysis. A system of computer programs to optimize and analyze skin-stringer panel for fuselage and lifting surfaces (wing and empennage structures) is being developed at the Institute of aerospace engineering, FME, BUT now. This paper deals with the optimum design of the reinforced panel which means Skin – stringer Panel. This form of construction is a logical development of the necessity of providing a continuous surface for an airplane, combined with the requirement that the weight of structure should be as small as possible.

English abstract

In modern aircraft structural design, the high accuracy calculation to obtain the highest efficiency of the structure is possible through the use of computer analysis. A system of computer programs to optimize and analyze skin-stringer panel for fuselage and lifting surfaces (wing and empennage structures) is being developed at the Institute of aerospace engineering, FME, BUT now. This paper deals with the optimum design of the reinforced panel which means Skin – stringer Panel. This form of construction is a logical development of the necessity of providing a continuous surface for an airplane, combined with the requirement that the weight of structure should be as small as possible.

Keywords in Czech

mathematical programming, optimization, stiffened panel

Keywords in English

mathematical programming, optimization, stiffened panel

RIV year

2006

Released

08.11.2006

Publisher

VZLU

Location

Praha

ISSN

1211-877X

Journal

Letecký zpravodaj

Volume

2006

Number

3

Pages from–to

42–45

Pages count

4

BIBTEX


@article{BUT43902,
  author="Miroslav {Pešák} and Antonín {Píštěk},
  title="OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING",
  journal="Letecký zpravodaj ",
  year="2006",
  volume="2006",
  number="3",
  month="November",
  pages="42--45",
  publisher="VZLU",
  address="Praha",
  issn="1211-877X"
}