Aircraft Design, Flicht Mechanics, Aircraft Systems. --- This dataverse contains research data and software produced by students for their projects and theses. --- Get linked to all other resources from their reports using the URN from the German National Library (DNB) as given in each dataset under "Metadata".
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1,411 to 1,420 of 1,453 Results
Projekt_Dennis_Lucht_2019.xlsx
Feb 26, 2020 - Überprüfung einer einfachen Kopfrechenmethode zur Umrechnung der Fluggeschwindigkeit von CAS in TAS
MS Excel Spreadsheet - 6.1 MB - MD5: efb00e12355974aba5a59d2c0b04817a
Basic Comparison of Three Aircraft Concepts: Classic Jet Propulsion, Turbo-Electric Propulsion and Turbo-Hydraulic Propulsion
Feb 11, 2020
Rodrigo, Clinton, 2020, "Basic Comparison of Three Aircraft Concepts: Classic Jet Propulsion, Turbo-Electric Propulsion and Turbo-Hydraulic Propulsion", https://doi.org/10.7910/DVN/K5FLHR, Harvard Dataverse, V1
Purpose - This paper presents a comparison of aircraft design concepts to identify the superior propulsion system model among turbo-hydraulic, turbo-electric and classic jet propulsion with respect to Direct Operating Costs (DOC), environmental impact and fuel burn. --- Approach - A simple aircraft model was designed based on the Top-Level Aircraft...
AircraftPremilinarySizing_Electric&HydraulicPropulsion-1.xlsm
Feb 11, 2020 - Basic Comparison of Three Aircraft Concepts: Classic Jet Propulsion, Turbo-Electric Propulsion and Turbo-Hydraulic Propulsion
application/vnd.ms-excel.sheet.macroEnabled.12 - 522.7 KB - MD5: f2dc1817ba75389679c461a0b6915f85
Conditions for Passenger Aircraft Minimum Fuel Consumption, Direct Operating Costs and Environmental Impact
Feb 7, 2020
Caers, Brecht, 2020, "Conditions for Passenger Aircraft Minimum Fuel Consumption, Direct Operating Costs and Environmental Impact", https://doi.org/10.7910/DVN/DLZSDK, Harvard Dataverse, V1
Purpose – Find optimal flight and design parameters for three objectives: minimum fuel consumption, Direct Operating Costs (DOC), and environmental impact of a passenger jet aircraft. --- Approach – Combining multiple models (this includes aerodynamics, specific fuel consumption, DOC, and equivalent CO2 mass) into one generic model. In this combine...
PassengerAircraftMinimumFuel.xlsm
Feb 7, 2020 - Conditions for Passenger Aircraft Minimum Fuel Consumption, Direct Operating Costs and Environmental Impact
application/vnd.ms-excel.sheet.macroEnabled.12 - 372.1 KB - MD5: a8e2e33db68926b1bf963ac9891346bf
Reverse Engineering of Passenger Jets – Classified Design Parameters
Feb 7, 2020
De Grave, Emiel, 2020, "Reverse Engineering of Passenger Jets – Classified Design Parameters", https://doi.org/10.7910/DVN/KPHTG7, Harvard Dataverse, V1
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 aeroplan...
Derivation_RE.pdf
Feb 7, 2020 - Reverse Engineering of Passenger Jets – Classified Design Parameters
Adobe PDF - 4.0 MB - MD5: 29dcc1aaaa5ab7c549ea1fec47f366a4
ReverseEngineering.xlsm
Feb 7, 2020 - Reverse Engineering of Passenger Jets – Classified Design Parameters
application/vnd.ms-excel.sheet.macroEnabled.12 - 304.0 KB - MD5: 4d22c947e666ee5655b3b4ee3d06b923
Fallbeispiele zum Reverse Engineering im Passagierflugzeugentwurf
Jan 28, 2020
Cheema, John Singh, 2020, "Fallbeispiele zum Reverse Engineering im Passagierflugzeugentwurf", https://doi.org/10.7910/DVN/DIDFZI, Harvard Dataverse, V1
Zweck – In dieser Bachelorarbeit werden die öffentlich nicht zugänglichen Technologieparameter von Passagierflugzeugen näherungsweise bestimmt. Das sind maximaler Auftriebsbeiwert bei Start und Landung, maximale Gleitzahl und spezifischer Kraftstoffverbrauch im Reiseflug. Folgende Flugzeuge werden paarweise untersucht und verglichen: A340-300 und I...
A319-100.xlsm
Jan 28, 2020 - Fallbeispiele zum Reverse Engineering im Passagierflugzeugentwurf
application/vnd.ms-excel.sheet.macroEnabled.12 - 305.8 KB - MD5: 1f5e2f7f42a88030e4c4db05b6f57683
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