2000 IEEE Aerospace Conference. Proceedings (Cat. No.00TH8484)
DOI: 10.1109/aero.2000.879412
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New approaches to high speed civil transport multidisciplinary design and optimization

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Cited by 7 publications
(4 citation statements)
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“…Both research groups concluded that flutter would be determined in the prototype development phase. 7 Zink et al go on to state that it is at this early design stage that the complex problem can be most effectively and economically addressed. Weisshaar puts it clearly as follows: consideration and prediction of aeroelastic effects are essential for the efficient design of high performance flight vehicles.…”
Section: Methods To Design For Aeroelasticitymentioning
confidence: 99%
“…Both research groups concluded that flutter would be determined in the prototype development phase. 7 Zink et al go on to state that it is at this early design stage that the complex problem can be most effectively and economically addressed. Weisshaar puts it clearly as follows: consideration and prediction of aeroelastic effects are essential for the efficient design of high performance flight vehicles.…”
Section: Methods To Design For Aeroelasticitymentioning
confidence: 99%
“…Multidisciplinary aircraft design and evaluation (MADE) is an integrated software facilitating the rapid developing of multidisciplinary applications for aerospace vehicles design [14]. DREAMS developed by Georgia Tech Aircraft System Design Lab has been applied successfully in the concept design and preliminary design stages of high-speed civil transport wing [15]. A distributed MDO platform which mainly resolves expensive data management and user collaborative problems was developed, and has been used for the missile design and optimization [16].…”
Section: A Non-commercial Mdo Frameworkmentioning
confidence: 99%
“…PROBABILISTIC METHODS AT THE ENGINEERING LEVEL -Much work has been done recently using probabilistic methods at the individual aerospace concepts level [13,14,15,16]. Metamodels based on regression methods have been created relating vehicle design variables (geometry, engine specifications, drag polars, etc) to vehicle responses (takeoff gross weight, thrust-to-weight ratio, etc.).…”
Section: Preliminary Investigationsmentioning
confidence: 99%
“…Monte Carlo Simulation -After determining shape distributions for all of the variables, a Monte Carlo simulation, utilizing the Crystal Ball [14] software, is conducted. Variable values are chosen randomly based on the distribution given.…”
Section: Figure 9-notional Shape Function For a Wing Weight Reduction...mentioning
confidence: 99%