Ohme, Per and Vechtel, Dennis (2010) Criticality and Sensitivity Analysis of a Hybrid Laminar Flow Control System on Aircraft Level. DLR-Interner Bericht. DLR-IB 111-2010/06, 101 S.
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This report describes the results of an analysis concerning criticality and sensitivity of a hybrid laminar flow control system on aircraft level. The work was performed by the DLR Institute of Flight Systems subcontracted by Airbus Deutschland. A hybrid laminar flow control system (HLFC) at both wings, horizontal and vertical stabilizer should improve aircraft performance by reducing drag at the specific surface. A suction system should be installed at the leading edge of wings and stabilizers to control a laminar flow. The report outlines the results of a parameter study performed for a twin engine long range aircraft in clean configuration. Benefits in aircraft performance due to the HLFC system and consequences of system failures were investigated.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||Criticality and Sensitivity Analysis of a Hybrid Laminar Flow Control System on Aircraft Level|
|Date:||25 January 2010|
|Number of Pages:||101|
|Keywords:||A330 Aircraft Model, Simulation of HLFC System Failures, Software Tool MAPET I, Hybrid Laminar Flow Control System|
|HGF - Research field:||other|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Systems & Cabin|
|Institutes and Institutions:||Institute of Flight Systems > Flight Dynamics and Simulation|
|Deposited By:||Tanja Bracke|
|Deposited On:||11 Mar 2010 12:45|
|Last Modified:||11 Mar 2010 12:45|
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