Reverse Engineering of Passenger Jets – Classified Design Parameters

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dc.identifier.uri http://dx.doi.org/10.15488/9322
dc.identifier.uri https://www.repo.uni-hannover.de/handle/123456789/9375
dc.contributor.advisor Scholz, Dieter
dc.contributor.author De Grave, Emiel ger
dc.date.accessioned 2020-02-10T10:05:55Z
dc.date.issued 2017
dc.identifier.citation De Grave, Emiel: Reverse Engineering of Passenger Jets – Classified Design Parameters. Master Thesis. Hamburg : Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences, 2017. URN: https://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2017-08-25.017 ger
dc.description.abstract This thesis explains how the classified design parameters of existing passenger jets can be determined. The classified design parameters are; the maximum lift coefficient for landing and take-off, the maximum aerodynamic efficiency and the specific fuel consumption. The entire concept is based on the preliminary sizing of jet powered civil aeroplanes. This preliminary sizing is explained in detail because it is the foundation of the final result. The preliminary sizing is combined using reverse engineering which is not a strict method. Therefore, only the basics are explained. By applying reverse engineering on the preliminary sizing and aiming for the classified design parameters as output, formulas are derived to calculate the maximum lift coefficients, the maximum aerodynamic efficiency and the specific fuel consumption. The goal is to calculate these parameters, using only aircraft specifications that are made public by the manufacturer. The calculations are complex with mutual relations, iterative processes and optimizations. Therefore, it is interesting to integrate everything in a tool. The tool is built in Microsoft Excel and explained in detail adding operating instructions. The program is executed for miscellaneous aeroplanes, supported with the necessary comments. Investigated aeroplanes are: Caravelle 10B (Sud-Aviation), Boeing 707-320C, BAe 146-200 (British Aerospance), A320-200 (Airbus), "The Rebel" (based on A320), Boeing SUGAR High, Boeing 747-400, Blended Wing Body VELA 2 (VELA) and Dassault Falcon 8X. eng
dc.language.iso eng ger
dc.publisher Hamburg : Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences
dc.relation.requires https://doi.org/10.7910/DVN/KPHTG7
dc.rights CC BY-NC-SA 4.0 Unported ger
dc.rights.uri https://creativecommons.org/licenses/by-nc-sa/4.0 ger
dc.subject Preliminary sizing eng
dc.subject Glide ratio eng
dc.subject L/D eng
dc.subject Cruise eng
dc.subject Reiseflug ger
dc.subject Gleitzahl ger
dc.subject Auftriebsbeiwert ger
dc.subject.classification Luftfahrt ger
dc.subject.classification Luftfahrzeug ger
dc.subject.classification Passagierflugzeug ger
dc.subject.classification Reverse Engineering ger
dc.subject.classification Luftfahrttechnik ger
dc.subject.classification Aerodynamik ger
dc.subject.classification Passagier ger
dc.subject.classification Flugzeug ger
dc.subject.classification Entwurf ger
dc.subject.classification Dimensionierung ger
dc.subject.classification Verifikation ger
dc.subject.classification Kraftstoffverbrauch ger
dc.subject.classification Start ger
dc.subject.classification Landung ger
dc.subject.ddc 600 | Technik ger
dc.subject.ddc 620 | Ingenieurwissenschaften und Maschinenbau ger
dc.subject.ddc 629,1 | Luft- und Raumfahrttechnik ger
dc.subject.lcsh Aeronautics eng
dc.subject.lcsh Airplanes eng
dc.subject.lcsh Design eng
dc.subject.lcsh Reverse engineering eng
dc.subject.lcsh Aerodynamics eng
dc.subject.lcsh Aeroplanes eng
dc.subject.lcsh Computer software eng
dc.subject.lcsh Electronic spreadsheets eng
dc.subject.lcsh Verification (Logic) eng
dc.subject.lcsh Airplanes--Fuel consumption eng
dc.subject.lcsh Lift (Aerodynamics) eng
dc.subject.lcsh Airplanes—Takeoff eng
dc.subject.lcsh Airplanes—Landing eng
dc.title Reverse Engineering of Passenger Jets – Classified Design Parameters ger
dc.type book ger
dc.type masterThesis ger
dc.type Text ger
dc.relation.urn https://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2017-08-25.017
dc.relation.other https://n2t.net/ark:/13960/t5m98q09x
dc.description.version publishedVersion ger
tib.accessRights frei zug�nglich ger


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