Data underlying the MSc thesis: Development of a Cessna Skymaster mathematical model

DOI:10.4121/a74d4324-ce07-45a9-9e9a-d4177e733a0b.v1
The DOI displayed above is for this specific version of this dataset, which is currently the latest. Newer versions may be published in the future. For a link that will always point to the latest version, please use
DOI: 10.4121/a74d4324-ce07-45a9-9e9a-d4177e733a0b

Datacite citation style

Wiącek, Jan (2025): Data underlying the MSc thesis: Development of a Cessna Skymaster mathematical model. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/a74d4324-ce07-45a9-9e9a-d4177e733a0b.v1
Other citation styles (APA, Harvard, MLA, Vancouver, Chicago, IEEE) available at Datacite

Dataset

Dataset supporting the master thesis: Development of a Cessna Skymaster mathematical model: A Two Step method aerodynamic and engine model identification from flight test data. Includes flight test data, Matlab code, supporting performance data and figures. The structure is documented with README.txt files.

History

  • 2025-10-20 first online, published, posted

Publisher

4TU.ResearchData

Format

Matlab code (.m), flight test data (.hdf5, .csv, .m), propeller efficiency charts (.eta, .pitch, .ct), figures (.png), digital DATCOM input (.inp) and output (.out), README files (.txt)

Organizations

TU Delft, Faculty of Aerospace Engineering, Flight Performance and Propulsion

DATA

Files (1)