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Aviation and the Global Atmosphere

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<strong>Aviation</strong> <strong>and</strong> <strong>the</strong> <strong>Global</strong> <strong>Atmosphere</strong><br />

<strong>Aviation</strong> <strong>and</strong> <strong>the</strong> <strong>Global</strong> <strong>Atmosphere</strong><br />

Table of contents | Previous page | Next page<br />

7.3. Airframe Performance <strong>and</strong> Technology<br />

O<strong>the</strong>r reports in this collection<br />

Historically, efforts to improvement aerodynamic efficiency have been aimed mainly at two phases of flight: Take-off/climb <strong>and</strong> cruise. To this end, significant<br />

improvements in lift <strong>and</strong> drag performance have been achieved (Lynch et al., 1996). A comprehensive range of detailed aerodynamic studies, examining all aspects of<br />

<strong>the</strong> complex flows around <strong>the</strong> airframe, has been a major part of <strong>the</strong>se efforts. Such work, involving <strong>the</strong> development <strong>and</strong> use of high fidelity computational fluid<br />

dynamics (CFD) prediction codes (Rubbert, 1994) coupled with improved wind tunnel testing techniques (Lynch <strong>and</strong> Crites, 1996), has led to much better<br />

underst<strong>and</strong>ing of <strong>the</strong> aerodynamic characteristics of new <strong>and</strong> proposed designs. In turn, this work has led naturally to improved predictions of <strong>the</strong> effectiveness of<br />

measures aimed at improving <strong>the</strong> performance of aircraft in general <strong>and</strong> reducing fuel burn rates for future aircraft in particular.<br />

7.3.1. Aerodynamic Improvement<br />

Historically, efforts to improvement aerodynamic efficiency have been aimed mainly at two phases of flight: Take-off/climb <strong>and</strong> cruise. To this end, significant<br />

improvements in lift <strong>and</strong> drag performance have been achieved (Lynch et al., 1996). A comprehensive range of detailed aerodynamic studies, examining all aspects of<br />

<strong>the</strong> complex flows around <strong>the</strong> airframe, has been a major part of <strong>the</strong>se efforts. Such work, involving <strong>the</strong> development <strong>and</strong> use of high fidelity computational fluid<br />

dynamics (CFD) prediction codes (Rubbert, 1994) coupled with improved wind tunnel testing techniques (Lynch <strong>and</strong> Crites, 1996), has led to much better<br />

underst<strong>and</strong>ing of <strong>the</strong> aerodynamic characteristics of new <strong>and</strong> proposed designs. In turn, this work has led naturally to improved predictions of <strong>the</strong> effectiveness of<br />

measures aimed at improving <strong>the</strong> performance of aircraft in general <strong>and</strong> reducing fuel burn rates for future aircraft in particular.<br />

7.3.2. Airframe Weight Reduction<br />

The increasing availability of advanced lighter <strong>and</strong> stronger materials for use in structural components of <strong>the</strong> airframe has also been a major factor in <strong>the</strong> achievement<br />

of reduced fuel burn. Of particular note are <strong>the</strong> greater use of new aluminum alloys, titanium components, <strong>and</strong> composite materials for secondary (non-load-bearing)<br />

structures.<br />

One of <strong>the</strong> important enabling technologies that has had a major impact on <strong>the</strong>se developments is high-fidelity finite element models (FEMs). FEMs are now<br />

http://www.ipcc.ch/ipccreports/sres/aviation/093.htm (1 von 3)08.05.2008 02:43:23

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