Detail publikace

OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING

PEŠÁK, M. PÍŠTĚK, A.

Český název

OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING

Anglický název

OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING

Typ

článek v časopise - ostatní, Jost

Jazyk

cs

Originální abstrakt

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.

Český abstrakt

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.

Anglický abstrakt

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.

Klíčová slova česky

mathematical programming, optimization, stiffened panel

Klíčová slova anglicky

mathematical programming, optimization, stiffened panel

Rok RIV

2006

Vydáno

08.11.2006

Nakladatel

VZLU

Místo

Praha

ISSN

1211-877X

Časopis

Letecký zpravodaj

Ročník

2006

Číslo

3

Strany od–do

42–45

Počet stran

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"
}