Aerospace
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Item Open Access A Benchtop Flight Control Demonstrator - Data and Code(Cranfield University, 2019-09-10 09:28) Duran, Joris; Whidborne, James; Pontillo, Alessandro; alejandro Carrizales rodriguez, MartinCodes and data for "A benchtop flight control demonstrator" J R Duran, J F Whidborne, M Carrizales Rodriguez, A Pontillo International Journal of Mechanical Engineering Education Published online July 27, 2019 doi: 10.1177/0306419019852688CodesFlight-Desk-Control-Demonstrator-master.zip - GUI on a computer programmed in JAVA - PID Controller for ArduinoExperimental Results- Test open loop.xls- Test P.xls- Test PID.xlsFluent CFD Fileswindtunnel.casWindtunnel.jouWindtunnel_refine.meshdatJavaFoil filescriptJaveFoilMicrosoft Excel Windtunnel design worksheetWind Tunnel Design V2.xlsmCATIA CAD filesCAD-CATIA.zipMSc DissertationDuran JR. Flight Desk Control Demonstrator. MSc dissertation, Cranfield University, Bedfordshire, U.K., 2018. Available at: http://dspace.lib.cranfield.ac.uk/handle/1826/14154Item Open Access 'A Holistic Cabin Conceptualisation Approach (HCCA) framework'(Cranfield University, 2023-11-01 09:50) Kirensky, Roman; Lawson, Craig; Orson, BenThe presented toolset defines the stakeholders involved in aircraft passenger cabin interior development projects, and their pursued design drivers. - Stakeholder Definition sheet presents all types of organisations involved in the design of aircraft cabin interiors, disregarding of the involvement extent. - Stakeholder Analysis sheet contains the pairwise comparison matrices for all stakeholders along the influence and interest axes, and the resulting plot. - Cabin Design Drivers sheet contains the definition of drivers pursued by the cabin interior projects. These are defined as a multi-level structure including: -- Top-level profitability-based design drivers, -- Their constituent factors representing the design considerations and themes, and -- Bottom-level design criteria representing the detailed product specifications, requirements, features, qualities, performance targets etc. - Design Factor Weights present a set of pairwise comparison matrices for deriving the relative importance weights at the factor and driver levels. - R Input sheet contains R code template to use with R Studio software to retrieve Eigenvector values. - Design Factors Map sheet contains factor applicability mapping to represent stakeholder concern and interaction points on a cabin interior project. - Cabin Product Breakdown sheet presents the composition of state-of-the-art cabin interiors by listing out the components it may have. The presented list is an all-encompassing version and does not represent the product line of any specific cabin manufacturer or equipment supplier. The presented sheets may be used as information source, or be amended to reflect the needs of their specific project. Amendments may be performed in the white cells of the pairwise comparison matrices on Stakeholder Analysis and Design Factor Weights; and applicability indicators in Design Factors Map and Cabin Product Breakdown sheets.Item Open Access Air jet flow control on pitching aerofoils(Cranfield University, 2019-07-08 09:09) Prince, Simon; Green, Richard; Khodaglian, VahikExperimental data on the effect of steady and pulsed air jet vortex generator blowing on a RAE9645 aerofoil section in dynamic stall.Item Open Access Airport Operation Frequency Analysis(Cranfield University, 2023-08-21 09:28) Hin Pang, ChiThis spreadsheet is the airport operation frequency analysis performed using data from EuroControl Onesky.Item Open Access Blended wing body design and analysis(Cranfield University, 2024-05-23 12:45) Chan, Joseph; Sun, Yicheng; Smith, HowardData collected from different simulations and analyses calculated using GENUSItem Open Access British Airways Analysed Flight Data(Cranfield University, 2023-08-21 09:26) Hin Pang, ChiThese files are generated by the Analysis Python Program. They contain information for calculating taxi energy in each flight file.Item Open Access British Airways Analysis Output Files(Cranfield University, 2023-08-21 09:26) Hin Pang, ChiThese files are the CSV and word files generated by the "Taxi Time and Energy Analysis Python Program" automatically. It concludes the taxi time and taxi energy found by the program under different models of aircraft.Item Open Access British Airways File Lists(Cranfield University, 2023-08-21 09:25) Hin Pang, ChiThese files are the inputs of files to the "Taxi Time and Energy Analysis Python Program". They should be filled in by users with the flight data that needs to be analysed and be placed in the same folder as the Python Program. The particular column of "File Name" should contain the exact file name of flight data csv file. Otherwise, the "Taxi Time and Energy Analysis Python Program" would not be able to locate the flight file and perform analysis.Item Open Access British Airways Raw Flight Data(Cranfield University, 2023-08-21 09:26) Hin Pang, ChiThese files are extracted from FlightRadar24 which contains information to be extracted with the Analysis Python Program. They should be placed in the same folder as the Python Program to ensure the analysis can be done. Please do not share the files without having consent from FlightRadar24.Item Open Access Case studies for alternative fuels in different aircraft configurations(Cranfield University, 2024-05-24 13:09) Chan, Joseph; Sun, Yicheng; Howard,PeterResults of three case studies for different aircraft configurations, tube-and-wing, high aspect ratio wing and blended wing body, using different alternative fuels, kerosene based jet fuel, biofuel, ammonia, liquefied natural gas and liquid hydrogen.Item Open Access Civil Transport Aircraft Evolvability Data(Cranfield University, 2018-10-15 13:44) Van Heerden, Stevan; Guenov, Marin; Molina-Cristobal, ArturoThis is an appendix to the paper `Evolvability and Design Reuse in Civil Jet Transport Aircraft', by A.S.J. van Heerden, Marin D. Guenov, and Arturo Molina-Cristobal. It contains data that was used to create the plots and figures in Sections 6, 7, and 8 of the paper.Item Open Access Cranfield DrivAer] CAD_Pack_1 Main Body(Cranfield University, 2018-04-10 16:30) Francisco Soares, Renan; Garry, Kevin; Holt, JennyMain Body CAD Pack (35% scaled-version), including:1. DrivAer_hp - Main_body (S):Main-body surface, with two cuttings for Rear-end and Diffuser CAD Pack.2. DrivAer_hp - Main_body (S) (diffuser lid):'Diffuser lid' surface, which matches the Main-body's Diffuser cutting in order to complete the Main-body, smooth underfloor version (S).CAD files available in IGS, STEP, STL, and Parasolid formats. All geometries are provided in [mm].Notation:(S) = [modified] Smooth Underfloor CAD designed and uploaded by:Renan F Soares - PhD in Aerospace Applied Aerodynamics Group Cranfield University, United KingdomItem Open Access [Cranfield DrivAer] CAD_Pack_2 Rear-end (Standard DrivAer)(Cranfield University, 2018-04-10 16:30) Francisco Soares, Renan; Garry, Kevin; Holt, JennyRear-end CAD Pack (35% scaled-version), including:1. DrivAer - Rear-end Fastback (F):Rear-end surface equivalent to a generic Fastback car model.2. DrivAer - Rear-end Notchback (N):Rear-end surface equivalent to a generic Notchback car model.3. DrivAer - Rear-end Estateback (E):Rear-end surface equivalent to a generic Estateback car model.CAD files available in IGS, STEP, STL, and Parasolid formats. All geometries are provided in [mm].Notation:(F) = Fastback(N) = Notchback(E) = EstatebackReference:1. DrivAer Model : “Geometry”. Institute of Aerodynamics and Fluid Mechanics. Technical University of Munich. http://www.aer.mw.tum.de/en/research-groups/automotive/ drivaer/geometry/.-CAD adapted and uploaded by:Renan F Soares - PhD in AerospaceApplied Aerodynamics GroupCranfield University, United KingdomItem Open Access [Cranfield DrivAer] CAD_Pack_3 Mirrors(Cranfield University, 2018-04-10 16:30) Francisco Soares, Renan; Garry, Kevin; Holt, JennyMirrors CAD Pack (35% scaled-version), including:1. DrivAer - Mirrors (base plate only) (woM):DrivAer mirrors, base plate only.2. DrivAer - Mirrors (standard) (wM):DrivAer mirrors, standard version.CAD files available in IGS, STEP, STL, and Parasolid formats. All geometries are provided in [mm].Notation:(woM) = without external mirrors.(wM) = with external mirrors. --CAD designed and uploaded by:Renan F Soares - PhD in Aerospace Applied Aerodynamics Group Cranfield University, United KingdomItem Open Access [Cranfield DrivAer] CAD_Pack_6 Strakes(Cranfield University, 2018-04-10 16:32) Francisco Soares, Renan; Knowles, Andrew; Garry, Kevin; Holt, JennyStrakes CAD Pack (35% scaled-version), including:1. DrivAer_hp - Strakes (Lower-pair S-size):Lower pair of strakes, in nominal Small size.2. DrivAer_hp - Strakes (Lower-pair M-size):Lower pair of strakes, in nominal Medium size.3. DrivAer_hp - Strakes (Lower-pair L-size):Lower pair of strakes, in nominal Large size.4. DrivAer_hp - Strakes (Upper-pair S-size):Upper pair of strakes, in nominal Small size.5. DrivAer_hp - Strakes (Upper-pair M-size):Upper pair of strakes, in nominal Medium size.6. DrivAer_hp - Strakes (Upper-pair L-size):Upper pair of strakes, in nominal Large size.CAD files available in IGS, STEP, STL, and Parasolid formats. All geometries are provided in [mm].Notation:(Lower-set) = lower pais of strakes.(Upper-set) = upper pais of strakes.(Full-set) = both lower and upper pairs of strakes. CAD designed and uploaded by: Renan F Soares - PhD in Aerospace Applied Aerodynamics Group Cranfield University, United KingdomItem Open Access [Cranfield DrivAer] CAD_Pack_7 Spoilers(Cranfield University, 2018-04-10 16:32) Francisco Soares, Renan; Golons Olives, Sergio; Garry, Kevin; Holt, JennySpoilers CAD Pack (35% scaled-version), including:1. DrivAer_hp - Spoiler (spL040 spA40): Spoiler pack with plate size of 40 mm, set at 40 deg.2. DrivAer_hp - Spoiler (spL080 spA40):Spoiler pack with plate size of 80 mm, set at 40 deg.3. DrivAer_hp - Spoiler (spL120 spA40):Spoiler pack with plate size of 120 mm, set at 40 deg.4. DrivAer_hp - Spoiler (spL080 spA20):Spoiler pack with plate size of 80 mm, set at 20 deg.5. DrivAer_hp - Spoiler (spL080 spA60):Spoiler pack with plate size of 80 mm, set at 60 deg.CAD files available in IGS, STEP, STL, and Parasolid formats. All geometries are provided in [mm].Notation:(spL) = length of the spoiler plate.(spA) = angle of the spoiler plate, in reference to the ground. CAD designed and uploaded by:Renan F Soares - PhD in AerospaceApplied Aerodynamics GroupCranfield University, United KingdomItem Open Access [Cranfield DrivAer] CAD_Pack_8 Diffusers(Cranfield University, 2018-04-10 16:33) Francisco Soares, Renan; Goñalons Olives, Sergio; Garry, Kevin; Holt, JennyDiffusers CAD Pack (35% scaled-version), including:1. DrivAer_hp - Diffuser (side plates):Side plates used to generate an diffuser channel for slopping angles protruding the DrivAer main body (i.e. diffA < 7 deg).2. DrivAer_hp - Diffuser (diffA00 plain):Diffuser pack with a plain, sloping surface of 0 deg (i.e. 'no-diffuser' case).3. DrivAer_hp - Diffuser (diffA05 plain):Diffuser pack with a plain, sloping surface of 5 deg.4. DrivAer_hp - Diffuser (diffA10 plain):Diffuser pack with a plain, sloping surface of 10 deg.5. DrivAer_hp - Diffuser (diffA16 plain):Diffuser pack with a plain, sloping surface of 16 deg.6. DrivAer_hp - Diffuser (diffA05 SEP_on):Diffuser pack with a plain, sloping surface of 5 deg and 3 equidistant separators ('fins').7. DrivAer_hp - Diffuser (diffA10 SEP_on):Diffuser pack with a plain, sloping surface of 10 deg and 3 equidistant separators ('fins').8. DrivAer_hp - Diffuser (diffA16 SEP_on):Diffuser pack with a plain, sloping surface of 16 deg and 3 equidistant separators ('fins').CAD files available in IGS, STEP, STL, and Parasolid formats. All geometries are provided in [mm].Notation:(diffA) = nominal diffuser angle.(SEP_on) = use of longitudinal separators ('fins').-------------------------------------------------CAD designed and uploaded by:Renan F Soares - PhD in AerospaceApplied Aerodynamics GroupCranfield University, United KingdomItem Open Access Data for Paper "Numerical Investigation of Orifice Nearfield Flow Development in Oleo-Pneumatic Shock Absorbers"(Cranfield University, 2022-02-18 09:57) Sheikh Al Shabab, Ahmed; Skote, Martin; Tsoutsanis, Panagiotis; Antoniadis, Antonios; Vitlaris, Dimitrios; Grenko, BojanData for the journal paper titled: Numerical Investigation of Orifice Nearfield Flow Development in Oleo-Pneumatic Shock AbsorbersItem Open Access Data for Paper "Unsteady Multiphase Simulation of Oleo-Pneumatic Shock Absorber Flow"(Cranfield University, 2024-02-21 18:05) Sheikh Al Shabab, Ahmed; Grenko, Bojan; Silva, Paulo; Antoniadis, Antonios; Tsoutsanis, Panagiotis; Skote, MartinDataset for the paper "Unsteady Multiphase Simulation of Oleo-Pneumatic Shock Absorber Flow"Item Open Access Data for the paper "Inter-fibre failure of through-thickness reinforced laminates..."(Cranfield University, 2018-06-18 13:00) Cui, Hao; Yasaee, MehdiData used in the paper " Hao Cui, Antonio R. Melro, Mehdi Yasaee, Inter-fibre failure of through-thickness reinforced laminates in combined transverse compression and shear load, Composites Science and Technology, 2018 "
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